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A

a - Variable in class org.orekit.tle.TLEPropagator
final semi major axis.
a0dp - Variable in class org.orekit.tle.TLEPropagator
original recovered semi major axis.
AbsoluteDate - Class in org.orekit.time
This class represents a specific instant in time.
AbsoluteDate() - Constructor for class org.orekit.time.AbsoluteDate
Create an instance with a default value (AbsoluteDate.J2000_EPOCH).
AbsoluteDate(String, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location (parsed from a string) in a time scale.
AbsoluteDate(DateTimeComponents, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(DateComponents, TimeComponents, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(int, int, int, int, int, double, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(DateComponents, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(int, int, int, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(Date, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(AbsoluteDate, double) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from an elapsed duration since to another instant.
AbsoluteDate(AbsoluteDate, double, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from an apparent clock offset with respect to another instant in the perspective of a specific time scale.
ABSORPTION_COEFFICIENT - Static variable in class org.orekit.forces.radiation.SolarRadiationPressure
Parameter name for absorption coefficient enabling jacobian processing.
AbstractCelestialBody - Class in org.orekit.bodies
Abstract implementation of the CelestialBody interface.
AbstractCelestialBody(double, Frame) - Constructor for class org.orekit.bodies.AbstractCelestialBody
Build an instance using an existing body-centered frame.
AbstractCelestialBody(double, String, Frame) - Constructor for class org.orekit.bodies.AbstractCelestialBody
Build an instance and the underlying frame.
AbstractDetector - Class in org.orekit.propagation.events
Common parts shared by several orbital events finders.
AbstractDetector(double, double) - Constructor for class org.orekit.propagation.events.AbstractDetector
Build a new instance.
AbstractEOPHistory - Class in org.orekit.frames
This class loads any kind of Earth Orientation Parameter data throughout a large time range.
AbstractEOPHistory() - Constructor for class org.orekit.frames.AbstractEOPHistory
Simple constructor.
AbstractPropagator - Class in org.orekit.propagation
Common handling of Propagator methods for analytical-like propagators.
AbstractPropagator() - Constructor for class org.orekit.propagation.AbstractPropagator
Build a new instance.
AdaptedEventDetector - Class in org.orekit.propagation.events
Adapt an EventDetector to commons-math EventHandler interface.
AdaptedEventDetector(EventDetector, AbsoluteDate, double, Frame, AttitudeLaw) - Constructor for class org.orekit.propagation.events.AdaptedEventDetector
Build a wrapped event detector.
AdaptedStepHandler - Class in org.orekit.propagation.sampling
Adapt an OrekitStepHandler to commons-math StepHandler interface.
AdaptedStepHandler(OrekitStepHandler) - Constructor for class org.orekit.propagation.sampling.AdaptedStepHandler
Build an instance.
addAcceleration(Vector3D, Frame) - Method in class org.orekit.propagation.numerical.TimeDerivativesEquations
Add the contribution of an acceleration expressed in some inertial frame.
addCelestialBodyLoader(String, CelestialBodyLoader) - Static method in class org.orekit.bodies.CelestialBodyFactory
Add a loader for celestial bodies.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.drag.DragForce
Compute the contribution of the drag to the perturbing acceleration.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in interface org.orekit.forces.ForceModel
Compute the contribution of the force model to the perturbing acceleration.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.gravity.CunninghamAttractionModel
Compute the contribution of the force model to the perturbing acceleration.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.gravity.DrozinerAttractionModel
Compute the contribution of the force model to the perturbing acceleration.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction
Compute the contribution of the force model to the perturbing acceleration.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Compute the contribution of the force model to the perturbing acceleration.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Compute the contribution of the force model to the perturbing acceleration.
addContributionWithJacobians(SpacecraftState, TimeDerivativesEquationsWithJacobians) - Method in class org.orekit.forces.drag.DragForce
Compute the contribution of the force model to the perturbing acceleration and to the jacobians.
addContributionWithJacobians(SpacecraftState, TimeDerivativesEquationsWithJacobians) - Method in interface org.orekit.forces.ForceModelWithJacobians
Compute the contribution of the force model to the perturbing acceleration and to the jacobians.
addContributionWithJacobians(SpacecraftState, TimeDerivativesEquationsWithJacobians) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Compute the contribution of the force model to the perturbing acceleration and to the jacobians.
addDefaultCelestialBodyLoader(String) - Static method in class org.orekit.bodies.CelestialBodyFactory
Add the default loaders for all predefined celestial bodies.
addDefaultCelestialBodyLoader(String, String) - Static method in class org.orekit.bodies.CelestialBodyFactory
Add the default loaders for celestial bodies.
addDefaultEOP1980HistoryLoaders(String, String) - Static method in class org.orekit.frames.FramesFactory
Add the default loaders for EOP 1980 history.
addDefaultEOP2000HistoryLoaders(String, String) - Static method in class org.orekit.frames.FramesFactory
Add the default loaders for EOP 2000 history.
addDefaultPotentialCoefficientsReaders() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Add the default READERS for gravity fields.
addDefaultProviders() - Method in class org.orekit.data.DataProvidersManager
Add the default providers configuration.
addDefaultUTCTAILoader() - Static method in class org.orekit.time.TimeScalesFactory
Add the default loader for UTC-TAI offsets history files.
addEndDateChecker(AbsoluteDate, AbsoluteDate, CombinedEventsDetectorsManager) - Method in class org.orekit.propagation.AbstractPropagator
Add an event handler for end date checking.
addEntry(EOP1980Entry) - Method in class org.orekit.frames.EOP1980History
Add an Earth Orientation Parameters entry.
addEntry(EOP2000Entry) - Method in class org.orekit.frames.EOP2000History
Add an Earth Orientation Parameters entry.
addEOP1980HistoryLoader(EOP1980HistoryLoader) - Static method in class org.orekit.frames.FramesFactory
Add a loader for EOP 1980 history.
addEOP2000HistoryLoader(EOP2000HistoryLoader) - Static method in class org.orekit.frames.FramesFactory
Add a loader for EOP 2000 history.
adder - Variable in class org.orekit.propagation.numerical.NumericalPropagator
Gauss equations handler.
addEventDetector(EventDetector) - Method in class org.orekit.propagation.AbstractPropagator
Add an event detector.
addEventDetector(EventDetector) - Method in class org.orekit.propagation.events.CombinedEventsDetectorsManager
Add an event detector.
addEventDetector(EventDetector) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Add an event detector.
addEventDetector(EventDetector) - Method in interface org.orekit.propagation.Propagator
Add an event detector.
addForceModel(ForceModel) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Add a force model to the global perturbation model.
addForceModel(ForceModel) - Method in class org.orekit.propagation.numerical.NumericalPropagatorWithJacobians
Add a force model to the global perturbation model.
addKeplerContribution() - Method in class org.orekit.propagation.numerical.TimeDerivativesEquations
Add the contribution of the Kepler evolution.
addMassDerivative(double) - Method in class org.orekit.propagation.numerical.TimeDerivativesEquations
Add the contribution of the flow rate (dm/dt).
addPotentialCoefficientsReader(PotentialCoefficientsReader) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Add a reader for gravity fields.
addPotentialReader(PotentialCoefficientsReader) - Method in class org.orekit.forces.gravity.potential.PotentialReaderFactory
Deprecated. Adds a PotentialCoefficientsReader to the test list.
addProvider(DataProvider) - Method in class org.orekit.data.DataProvidersManager
Add a data provider to the supported list.
addQSWAcceleration(double, double, double) - Method in class org.orekit.propagation.numerical.TimeDerivativesEquations
Add the contribution of an acceleration expressed in (q, s, w) local orbital frame.
addTNWAcceleration(double, double, double) - Method in class org.orekit.propagation.numerical.TimeDerivativesEquations
Add the contribution of an acceleration expressed in (t, n, w) local orbital frame.
addUTCTAILoader(UTCTAILoader) - Static method in class org.orekit.time.TimeScalesFactory
Add a loader for UTC-TAI offsets history files.
addXYZAcceleration(double, double, double) - Method in class org.orekit.propagation.numerical.TimeDerivativesEquations
Add the contribution of an acceleration expressed in the inertial frame (it is important to make sure this acceleration is defined in the same frame as the orbit) .
ae - Variable in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Central body reference radius.
AlignmentDetector - Class in org.orekit.propagation.events
Finder for satellite/body alignment events.
AlignmentDetector(Orbit, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AlignmentDetector
Build a new alignment detector.
AlignmentDetector(double, Orbit, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AlignmentDetector
Build a new alignment detector.
AltitudeDetector - Class in org.orekit.propagation.events
Finder for satellite altitude crossing events.
AltitudeDetector(double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector
Build a new altitude detector.
AltitudeDetector(double, double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector
Build a new altitude detector.
AltitudeDetector(double, double, double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector
Build a new altitude detector.
ApsideDetector - Class in org.orekit.propagation.events
Finder for apside crossing events.
ApsideDetector(Orbit) - Constructor for class org.orekit.propagation.events.ApsideDetector
Build a new instance.
ApsideDetector(double, Orbit) - Constructor for class org.orekit.propagation.events.ApsideDetector
Build a new instance.
argument(BodiesElements) - Method in class org.orekit.data.SeriesTerm
Compute the argument for the current date.
Atmosphere - Interface in org.orekit.forces.drag
Interface for atmospheric models.
ATOMIC_NITROGEN - Static variable in class org.orekit.forces.drag.DTM2000
Identifier for atomic nitrogen.
ATOMIC_OXYGEN - Static variable in class org.orekit.forces.drag.DTM2000
Identifier for atomic oxygen.
Attitude - Class in org.orekit.attitudes
This class handles attitude definition at a given date.
Attitude(AbsoluteDate, Frame, Rotation, Vector3D) - Constructor for class org.orekit.attitudes.Attitude
Creates a new instance.
AttitudeLaw - Interface in org.orekit.attitudes
This interface represents an attitude law model set.
attitudeLaw - Variable in class org.orekit.propagation.numerical.NumericalPropagator
Attitude law.

B

basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.AbstractPropagator
Propagate an orbit without any fancy features.
basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Propagate an orbit without any fancy features.
basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.KeplerianPropagator
Propagate an orbit without any fancy features.
BasicPropagator - Interface in org.orekit.propagation
This interface provides a way to propagate an orbit at any time.
BasicStepInterpolator - Class in org.orekit.propagation.sampling
Implementation of the OrekitStepInterpolator interface based on a BasicPropagator.
BasicStepInterpolator(BasicPropagator) - Constructor for class org.orekit.propagation.sampling.BasicStepInterpolator
Build a new instance from a basic propagator.
beta0 - Variable in class org.orekit.tle.TLEPropagator
sqrt (1 - e2).
beta02 - Variable in class org.orekit.tle.TLEPropagator
1 - e2.
BodiesElements - Class in org.orekit.data
Elements of the bodies having an effect on nutation.
BodiesElements(double, double, double, double, double, double, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.data.BodiesElements
Simple constructor.
BodyCenterPointing - Class in org.orekit.attitudes
This class handles body center pointing attitude law.
BodyCenterPointing(Frame) - Constructor for class org.orekit.attitudes.BodyCenterPointing
Creates new instance.
BodyShape - Interface in org.orekit.bodies
Interface representing the rigid surface shape of a natural body.
BoundedPropagator - Interface in org.orekit.propagation
This interface is intended for ephemerides valid only during a time range.
BoxAndSolarArraySpacecraft - Class in org.orekit.forces
experimental class representing the features of a classical satellite with a convex body shape and rotating flat solar arrays.
BoxAndSolarArraySpacecraft(double, double, double, PVCoordinatesProvider, double, Vector3D, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft
Build a spacecraft model with best lightning of solar array.
BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[], PVCoordinatesProvider, double, Vector3D, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft
Build a spacecraft model with best lightning of solar array.
BoxAndSolarArraySpacecraft(double, double, double, PVCoordinatesProvider, double, Vector3D, AbsoluteDate, Vector3D, double, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft
Build a spacecraft model with linear rotation of solar array.
BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[], PVCoordinatesProvider, double, Vector3D, AbsoluteDate, Vector3D, double, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft
Build a spacecraft model with linear rotation of solar array.
BoxAndSolarArraySpacecraft.Facet - Class in org.orekit.forces
Class representing a single facet of a convex spacecraft body.
BoxAndSolarArraySpacecraft.Facet(Vector3D, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft.Facet
Simple constructor.
buildTerm(double, double, int, int, int, int, int, int, int, int, int, int, int, int, int, int) - Static method in class org.orekit.data.SeriesTerm
Factory method for building the appropriate object.
BULLETINB_1980_FILENAME - Static variable in class org.orekit.frames.FramesFactory
Default regular expression for the BulletinB files (IAU1980 compatibles).
BULLETINB_2000_FILENAME - Static variable in class org.orekit.frames.FramesFactory
Default regular expression for the BulletinB files (IAU2000 compatibles).

C

c1 - Variable in class org.orekit.tle.TLEPropagator
C1 from SPTRCK #3.
c2 - Variable in class org.orekit.tle.TLEPropagator
C2 from SPTRCK #3.
c4 - Variable in class org.orekit.tle.TLEPropagator
C4 from SPTRCK #3.
calls - Variable in class org.orekit.propagation.numerical.NumericalPropagator
Counter for differential equations calls.
CartesianOrbit - Class in org.orekit.orbits
This class holds cartesian orbital parameters.
CartesianOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CartesianOrbit
Constructor from cartesian parameters.
CartesianOrbit(Orbit) - Constructor for class org.orekit.orbits.CartesianOrbit
Constructor from any kind of orbital parameters.
CelestialBody - Interface in org.orekit.bodies
Interface for celestial bodies like Sun, Moon or solar system planets.
CelestialBodyFactory - Class in org.orekit.bodies
Factory class for bodies of the solar system.
CelestialBodyLoader - Interface in org.orekit.bodies
Interface for loading celestial bodies.
CelestialBodyPointed - Class in org.orekit.attitudes
This class handles a celestial body pointed attitude law.
CelestialBodyPointed(Frame, PVCoordinatesProvider, Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.attitudes.CelestialBodyPointed
Creates new instance.
checkEOPContinuity(double) - Method in class org.orekit.frames.AbstractEOPHistory
Check Earth orientation parameters continuity.
ChronologicalComparator - Class in org.orekit.time
Comparator for TimeStamped instance.
ChronologicalComparator() - Constructor for class org.orekit.time.ChronologicalComparator
Simple constructor.
CircularFieldOfViewDetector - Class in org.orekit.propagation.events
Finder for target entry/exit events with respect to a satellite sensor field of view.
CircularFieldOfViewDetector(double, PVCoordinatesProvider, Vector3D, double) - Constructor for class org.orekit.propagation.events.CircularFieldOfViewDetector
Build a new instance.
CircularOrbit - Class in org.orekit.orbits
This class handles circular orbital parameters.
CircularOrbit(double, double, double, double, double, double, int, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit
Creates a new instance.
CircularOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit
Constructor from cartesian parameters.
CircularOrbit(Orbit) - Constructor for class org.orekit.orbits.CircularOrbit
Constructor from any kind of orbital parameters.
ClasspathCrawler - Class in org.orekit.data
Provider for data files stored as resources in the classpath.
ClasspathCrawler(String...) - Constructor for class org.orekit.data.ClasspathCrawler
Build a data classpath crawler.
clearCelestialBodyLoaders(String) - Static method in class org.orekit.bodies.CelestialBodyFactory
Clear loaders for one celestial body.
clearCelestialBodyLoaders() - Static method in class org.orekit.bodies.CelestialBodyFactory
Clear loaders for all celestial bodies.
clearEOP1980HistoryLoaders() - Static method in class org.orekit.frames.FramesFactory
Clear loaders for EOP 1980 history.
clearEOP2000HistoryLoaders() - Static method in class org.orekit.frames.FramesFactory
Clear loaders for EOP 2000 history.
clearEventsDetectors() - Method in class org.orekit.propagation.AbstractPropagator
Remove all events detectors.
clearEventsDetectors() - Method in class org.orekit.propagation.events.CombinedEventsDetectorsManager
Remove all the events detectors that have been added to the handler.
clearEventsDetectors() - Method in class org.orekit.propagation.numerical.NumericalPropagator
Remove all events detectors.
clearEventsDetectors() - Method in interface org.orekit.propagation.Propagator
Remove all events detectors.
clearPotentialCoefficientsReaders() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Clear gravity field READERS.
clearProviders() - Method in class org.orekit.data.DataProvidersManager
Remove all data providers.
clearUTCTAILoaders() - Static method in class org.orekit.time.TimeScalesFactory
Clear loaders for UTC-TAI offsets history files.
coef - Variable in class org.orekit.tle.TLEPropagator
coef for SGP C3 computation.
coef1 - Variable in class org.orekit.tle.TLEPropagator
coef for SGP C5 computation.
CombinedEventsDetectorsManager - Class in org.orekit.propagation.events
This class manages several event detectors during propagation.
CombinedEventsDetectorsManager() - Constructor for class org.orekit.propagation.events.CombinedEventsDetectorsManager
Simple constructor.
compare(TimeStamped, TimeStamped) - Method in class org.orekit.time.ChronologicalComparator
Compare two time-stamped instances.
compareTo(AbsoluteDate) - Method in class org.orekit.time.AbsoluteDate
Compare the instance with another date.
compareTo(DateComponents) - Method in class org.orekit.time.DateComponents
compareTo(DateTimeComponents) - Method in class org.orekit.time.DateTimeComponents
compareTo(TimeComponents) - Method in class org.orekit.time.TimeComponents
Constants - Interface in org.orekit.utils
Set of useful physical constants.
ConstantThrustManeuver - Class in org.orekit.forces.maneuvers
This class implements a simple maneuver with constant thrust.
ConstantThrustManeuver(AbsoluteDate, double, double, double, Vector3D) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver
Simple constructor for a constant direction and constant thrust.
contains(Vector3D) - Method in class org.orekit.utils.Line
Check if the instance contains a point.
CONTINUE - Static variable in interface org.orekit.propagation.events.EventDetector
Continue indicator.
cosi0 - Variable in class org.orekit.tle.TLEPropagator
cosinus original inclination.
createFromWeekComponents(int, int, int) - Static method in class org.orekit.time.DateComponents
Build a date from week components.
createGPSDate(int, double) - Static method in class org.orekit.time.AbsoluteDate
Build an instance corresponding to a GPS date.
createIllegalArgumentException(String, Object...) - Static method in exception org.orekit.errors.OrekitException
Create an IllegalArgumentException with localized message.
createIllegalStateException(String, Object...) - Static method in exception org.orekit.errors.OrekitException
Create an IllegalStateException with localized message.
createInternalError(Throwable) - Static method in exception org.orekit.errors.OrekitException
Create an RuntimeException for an internal error.
createParseException(String, Object...) - Static method in exception org.orekit.errors.OrekitException
Create an ParseException with localized message.
CunninghamAttractionModel - Class in org.orekit.forces.gravity
This class represents the gravitational field of a celestial body.
CunninghamAttractionModel(Frame, double, double, double[][], double[][]) - Constructor for class org.orekit.forces.gravity.CunninghamAttractionModel
Creates a new instance.
currentState - Variable in class org.orekit.propagation.numerical.NumericalPropagator
Current state to propagate.

D

DataLoader - Interface in org.orekit.data
Interface for loading data files from data providers.
DataProvider - Interface in org.orekit.data
Interface for providing data files to file loaders.
DataProvidersManager - Class in org.orekit.data
Singleton class managing all supported data providers.
DateComponents - Class in org.orekit.time
Class representing a date broken up as year, month and day components.
DateComponents(int, int, int) - Constructor for class org.orekit.time.DateComponents
Build a date from its components.
DateComponents(int, int) - Constructor for class org.orekit.time.DateComponents
Build a date from a year and day number.
DateComponents(int) - Constructor for class org.orekit.time.DateComponents
Build a date from its offset with respect to a DateComponents.J2000_EPOCH.
DateComponents(DateComponents, int) - Constructor for class org.orekit.time.DateComponents
Build a date from its offset with respect to a reference epoch.
DateDetector - Class in org.orekit.propagation.events
Finder for date events.
DateDetector(AbsoluteDate) - Constructor for class org.orekit.propagation.events.DateDetector
Build a new instance.
DateTimeComponents - Class in org.orekit.time
Holder for date and time components.
DateTimeComponents(DateComponents, TimeComponents) - Constructor for class org.orekit.time.DateTimeComponents
Build a new instance from its components.
DateTimeComponents(int, int, int, int, int, double) - Constructor for class org.orekit.time.DateTimeComponents
Build an instance from raw level components.
DateTimeComponents(int, int, int) - Constructor for class org.orekit.time.DateTimeComponents
Build an instance from raw level components.
DateTimeComponents(DateTimeComponents, double) - Constructor for class org.orekit.time.DateTimeComponents
Build an instance from a seconds offset with respect to another one.
DEFAULT - Static variable in class org.orekit.tle.TLE
Identifier for default type of ephemeris (SGP4/SDP4).
DEFAULT_MAXCHECK - Static variable in class org.orekit.propagation.events.AbstractDetector
Default maximum checking interval (s).
DEFAULT_THRESHOLD - Static variable in class org.orekit.propagation.events.AbstractDetector
Default convergence threshold (s).
detectors - Variable in class org.orekit.propagation.numerical.NumericalPropagator
Event detectors not related to force models.
DihedralFieldOfViewDetector - Class in org.orekit.propagation.events
Finder for body entering/exiting dihedral fov events.
DihedralFieldOfViewDetector(double, PVCoordinatesProvider, Vector3D, Vector3D, double, Vector3D, double) - Constructor for class org.orekit.propagation.events.DihedralFieldOfViewDetector
Build a new instance.
DirectoryCrawler - Class in org.orekit.data
Provider for data files stored in a directories tree on filesystem.
DirectoryCrawler(File) - Constructor for class org.orekit.data.DirectoryCrawler
Build a data files crawler.
distance(Vector3D) - Method in class org.orekit.utils.Line
Compute the distance between the instance and a point.
DRAG_COEFFICIENT - Static variable in class org.orekit.forces.drag.DragForce
Parameter name for drag coefficient enabling jacobian processing.
dragAcceleration(SpacecraftState, double, Vector3D) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Compute the acceleration due to drag.
dragAcceleration(SpacecraftState, double, Vector3D) - Method in interface org.orekit.forces.drag.DragSensitive
Compute the acceleration due to drag.
dragAcceleration(SpacecraftState, double, Vector3D) - Method in class org.orekit.forces.SphericalSpacecraft
Compute the acceleration due to drag.
DragForce - Class in org.orekit.forces.drag
Atmospheric drag force model.
DragForce(Atmosphere, DragSensitive) - Constructor for class org.orekit.forces.drag.DragForce
Simple constructor.
DragSensitive - Interface in org.orekit.forces.drag
Interface for spacecraft that are sensitive to atmospheric drag forces.
DrozinerAttractionModel - Class in org.orekit.forces.gravity
This class represents the gravitational field of a celestial body.
DrozinerAttractionModel(Frame, double, double, double[][], double[][]) - Constructor for class org.orekit.forces.gravity.DrozinerAttractionModel
Creates a new instance.
DTM2000 - Class in org.orekit.forces.drag
This atmosphere model is the realization of the DTM-2000 model.
DTM2000(DTM2000InputParameters, PVCoordinatesProvider, BodyShape, Frame) - Constructor for class org.orekit.forces.drag.DTM2000
Simple constructor for independent computation.
DTM2000InputParameters - Interface in org.orekit.forces.drag
Container for solar activity data, compatible with DTM2000 Atmosphere model.
dtN - Variable in class org.orekit.frames.AbstractEOPHistory
Offset to next date.
dtP - Variable in class org.orekit.frames.AbstractEOPHistory
Offset from previous date.
durationFrom(AbsoluteDate) - Method in class org.orekit.time.AbsoluteDate
Compute the physically elapsed duration between two instants.

E

e - Variable in class org.orekit.tle.TLEPropagator
final eccentricity.
e0sq - Variable in class org.orekit.tle.TLEPropagator
original eccentricity squared.
E_CIRC - Static variable in class org.orekit.orbits.KeplerianOrbit
Eccentricity threshold for near circular orbits.
EARTH - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Earth.
EARTH_MOON - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Earth-Moon barycenter.
ECCENTRIC_ANOMALY - Static variable in class org.orekit.orbits.KeplerianOrbit
Identifier for eccentric anomaly.
ECCENTRIC_LATITUDE_ARGUMENT - Static variable in class org.orekit.orbits.EquinoctialOrbit
Identifier for eccentric latitude argument.
ECCENTRIC_LONGITUDE_ARGUMENT - Static variable in class org.orekit.orbits.CircularOrbit
Identifier for eccentric longitude argument.
EcksteinHechlerPropagator - Class in org.orekit.propagation.analytical
This class propagates a SpacecraftState using the analytical Eckstein-Hechler model.
EcksteinHechlerPropagator(Orbit, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit and potential.
EcksteinHechlerPropagator(Orbit, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit, mass and potential.
EcksteinHechlerPropagator(Orbit, AttitudeLaw, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit, attitude law and potential.
EcksteinHechlerPropagator(Orbit, AttitudeLaw, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit, attitude law, mass and potential.
EclipseDetector - Class in org.orekit.propagation.events
Finder for satellite eclipse related events.
EclipseDetector(PVCoordinatesProvider, double, PVCoordinatesProvider, double, boolean) - Constructor for class org.orekit.propagation.events.EclipseDetector
Build a new eclipse detector.
EclipseDetector(double, PVCoordinatesProvider, double, PVCoordinatesProvider, double, boolean) - Constructor for class org.orekit.propagation.events.EclipseDetector
Build a new eclipse detector.
EclipseDetector(double, double, PVCoordinatesProvider, double, PVCoordinatesProvider, double, boolean) - Constructor for class org.orekit.propagation.events.EclipseDetector
Build a new eclipse detector .
EclipseDetector(PVCoordinatesProvider, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.EclipseDetector
Build a new eclipse detector.
EclipseDetector(double, PVCoordinatesProvider, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.EclipseDetector
Build a new eclipse detector.
EclipseDetector(double, double, PVCoordinatesProvider, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.EclipseDetector
Build a new eclipse detector.
eeta - Variable in class org.orekit.tle.TLEPropagator
original eccentricity * eta.
EGM96_EARTH_C20 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized second zonal coefficient from EGM96 model: -1.08262668355315e-3.
EGM96_EARTH_C30 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized third zonal coefficient from EGM96 model: 2.53265648533224e-6.
EGM96_EARTH_C40 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized fourth zonal coefficient from EGM96 model: 1.619621591367e-6.
EGM96_EARTH_C50 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized fifth zonal coefficient from EGM96 model: 2.27296082868698e-7.
EGM96_EARTH_C60 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized sixth zonal coefficient from EGM96 model: -5.40681239107085e-7.
EGM96_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth equatorial radius from EGM96 model: 6378136.3 m.
EGM96_EARTH_MU - Static variable in interface org.orekit.utils.Constants
Earth gravitational constant from EGM96 model: 3.986004415 m3/s2.
EGM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory
Default regular expression for EGM files.
EGMFormatReader - Class in org.orekit.forces.gravity.potential
This reader is adapted to the EGM Format.
EGMFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.EGMFormatReader
Simple constructor.
EIGEN5C_EARTH_C20 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized second zonal coefficient from EIGEN5C model: -1.082626457231767e-3.
EIGEN5C_EARTH_C30 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized third zonal coefficient from EIGEN5C model: 2.532547231862799e-6.
EIGEN5C_EARTH_C40 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized fourth zonal coefficient from EIGEN5C model: 1.619964434136e-6.
EIGEN5C_EARTH_C50 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized fifth zonal coefficient from EIGEN5C model: 2.277928487005437e-7.
EIGEN5C_EARTH_C60 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized sixth zonal coefficient from EIGEN5C model: -5.406653715879098e-7.
EIGEN5C_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth equatorial radius from EIGEN5C model: 6378136.46 m.
EIGEN5C_EARTH_MU - Static variable in interface org.orekit.utils.Constants
Earth gravitational constant from EIGEN5C model: 3.986004415 m3/s2.
ElevationDetector - Class in org.orekit.propagation.events
Finder for satellite raising/setting events.
ElevationDetector(double, TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationDetector
Build a new elevation detector.
ElevationDetector(double, double, TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationDetector
Build a new elevation detector.
ElevationDetector(double, double, double, TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationDetector
Build a new elevation detector.
EME2000_ALIGNED - Static variable in class org.orekit.attitudes.InertialLaw
Dummy attitude law, perfectly aligned with the EME2000 frame.
entries - Variable in class org.orekit.frames.AbstractEOPHistory
EOP history entries.
EOP1980Entry - Class in org.orekit.frames
This class holds an Earth Orientation Parameters entry (IAU1980).
EOP1980Entry(int, double, double, double, double) - Constructor for class org.orekit.frames.EOP1980Entry
Simple constructor.
EOP1980History - Class in org.orekit.frames
This class holds Earth Orientation Parameters (IAU1980) data throughout a large time range.
EOP1980History() - Constructor for class org.orekit.frames.EOP1980History
Simple constructor.
EOP1980HistoryLoader - Interface in org.orekit.frames
Interface for loading Earth Orientation Parameters 1980 history.
EOP2000Entry - Class in org.orekit.frames
This class holds an Earth Orientation Parameters entry (IAU2000).
EOP2000Entry(int, double, double, double, double) - Constructor for class org.orekit.frames.EOP2000Entry
Simple constructor.
EOP2000History - Class in org.orekit.frames
This class holds Earth Orientation Parameters (IAU2000) data throughout a large time range.
EOP2000History() - Constructor for class org.orekit.frames.EOP2000History
Simple constructor.
EOP2000HistoryLoader - Interface in org.orekit.frames
Interface for loading Earth Orientation Parameters 2000 history.
EOPC04_1980_FILENAME - Static variable in class org.orekit.frames.FramesFactory
Default regular expression for the EOPC04 files (IAU1980 compatibles).
EOPC04_2000_FILENAME - Static variable in class org.orekit.frames.FramesFactory
Default regular expression for the EOPC04 files (IAU2000 compatibles).
EOPEntry - Class in org.orekit.frames
This class holds an Earth Orientation Parameters entry.
EOPEntry(int, double, double) - Constructor for class org.orekit.frames.EOPEntry
Simple constructor.
EOPHistory - Interface in org.orekit.frames
Interface for retrieving Earth Orientation Parameters history throughout a large time range.
Ephemeris - Class in org.orekit.propagation
This class is designed to accept and handle tabulated orbital entries.
Ephemeris(SpacecraftState[]) - Constructor for class org.orekit.propagation.Ephemeris
Constructor with tabulated entries.
EPHEMERIS_GENERATION_MODE - Static variable in interface org.orekit.propagation.Propagator
Indicator for ephemeris generation mode.
equals(Object) - Method in class org.orekit.time.AbsoluteDate
Check if the instance represent the same time as another instance.
equals(Object) - Method in class org.orekit.time.DateComponents
equals(Object) - Method in class org.orekit.time.DateTimeComponents
equals(Object) - Method in class org.orekit.time.TimeComponents
EquinoctialOrbit - Class in org.orekit.orbits
This class handles equinoctial orbital parameters, which can support both circular and equatorial orbits.
EquinoctialOrbit(double, double, double, double, double, double, int, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit
Creates a new instance.
EquinoctialOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit
Constructor from cartesian parameters.
EquinoctialOrbit(Orbit) - Constructor for class org.orekit.orbits.EquinoctialOrbit
Constructor from any kind of orbital parameters.
estimateSpin(Rotation, Rotation, double) - Static method in class org.orekit.attitudes.Attitude
Estimate spin between two orientations.
estimateVelocity(Vector3D, Vector3D, double) - Static method in class org.orekit.utils.PVCoordinates
Estimate velocity between two positions.
eta - Variable in class org.orekit.tle.TLEPropagator
eta from SPTRCK #3.
etasq - Variable in class org.orekit.tle.TLEPropagator
eta squared.
evaluateStep(OrekitStepInterpolator) - Method in class org.orekit.propagation.events.CombinedEventsDetectorsManager
Evaluate the impact of the proposed step on all handled events detectors.
EventDetector - Interface in org.orekit.propagation.events
This interface represents space-dynamics aware events detectors.
eventOccurred(SpacecraftState, boolean) - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Handle an event and choose what to do next.
eventOccurred(SpacecraftState, boolean) - Method in class org.orekit.propagation.events.AbstractDetector
Handle an event and choose what to do next.
eventOccurred(double, double[], boolean) - Method in class org.orekit.propagation.events.AdaptedEventDetector
eventOccurred(SpacecraftState, boolean) - Method in class org.orekit.propagation.events.AlignmentDetector
Handle an alignment event and choose what to do next.
eventOccurred(SpacecraftState, boolean) - Method in class org.orekit.propagation.events.AltitudeDetector
Handle an altitude event and choose what to do next.
eventOccurred(SpacecraftState, boolean) - Method in class org.orekit.propagation.events.ApsideDetector
Handle an apside crossing event and choose what to do next.
eventOccurred(SpacecraftState, boolean) - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector
Handle an fov event and choose what to do next.
eventOccurred(SpacecraftState, boolean) - Method in class org.orekit.propagation.events.DateDetector
Handle a date event and choose what to do next.
eventOccurred(SpacecraftState, boolean) - Method in class org.orekit.propagation.events.DihedralFieldOfViewDetector
Handle an fov event and choose what to do next.
eventOccurred(SpacecraftState, boolean) - Method in class org.orekit.propagation.events.EclipseDetector
Handle an eclipse event and choose what to do next.
eventOccurred(SpacecraftState, boolean) - Method in class org.orekit.propagation.events.ElevationDetector
Handle an elevation event and choose what to do next.
eventOccurred(SpacecraftState, boolean) - Method in interface org.orekit.propagation.events.EventDetector
Handle an event and choose what to do next.
eventOccurred(SpacecraftState, boolean) - Method in class org.orekit.propagation.events.EventShifter
Handle an event and choose what to do next.
eventOccurred(SpacecraftState, boolean) - Method in class org.orekit.propagation.events.NodeDetector
Handle a node crossing event and choose what to do next.
EventShifter - Class in org.orekit.propagation.events
Wrapper shifting events occurrences times.
EventShifter(EventDetector, boolean, double, double) - Constructor for class org.orekit.propagation.events.EventShifter
Build a new instance.

F

feed(Pattern, DataLoader) - Method in class org.orekit.data.ClasspathCrawler
Feed a data file loader by browsing the data collection.
feed(Pattern, DataLoader) - Method in interface org.orekit.data.DataProvider
Feed a data file loader by browsing the data collection.
feed(String, DataLoader) - Method in class org.orekit.data.DataProvidersManager
Feed a data file loader by browsing all data providers.
feed(Pattern, DataLoader) - Method in class org.orekit.data.DirectoryCrawler
Feed a data file loader by browsing the data collection.
feed(Pattern, DataLoader) - Method in class org.orekit.data.NetworkCrawler
Feed a data file loader by browsing the data collection.
feed(Pattern, DataLoader) - Method in class org.orekit.data.ZipJarCrawler
Feed a data file loader by browsing the data collection.
FIFTIES_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for 1950 dates: 1950-01-01T00:00:00.
FIFTIES_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for 1950 dates: 1950-01-01.
fillHistory(EOP1980History) - Method in interface org.orekit.frames.EOP1980HistoryLoader
Load celestial body.
fillHistory(EOP2000History) - Method in interface org.orekit.frames.EOP2000HistoryLoader
Load celestial body.
FixedRate - Class in org.orekit.attitudes
This class handles a simple attitude law at constant rate around a fixed axis.
FixedRate(Attitude) - Constructor for class org.orekit.attitudes.FixedRate
Creates a new instance.
ForceModel - Interface in org.orekit.forces
This interface represents a force modifying spacecraft motion.
forceModels - Variable in class org.orekit.propagation.numerical.NumericalPropagator
Force models used during the extrapolation of the Orbit.
ForceModelWithJacobians - Interface in org.orekit.forces
This interface represents a parameterized force modifying spacecraft motion.
foundData() - Method in interface org.orekit.bodies.CelestialBodyLoader
Check if some data have already been loaded.
foundData() - Method in class org.orekit.bodies.JPLEphemeridesLoader
Check if some data have already been loaded.
Frame - Class in org.orekit.frames
Tridimensional references frames class.
Frame(Frame, Transform, String) - Constructor for class org.orekit.frames.Frame
Build a non-inertial frame from its transform with respect to its parent.
Frame(Frame, Transform, String, boolean) - Constructor for class org.orekit.frames.Frame
Build a frame from its transform with respect to its parent.
FrameAncestorException - Exception in org.orekit.errors
This class is the base class for exception thrown by the Frame.updateTransform method.
FrameAncestorException(String, Object...) - Constructor for exception org.orekit.errors.FrameAncestorException
Simple constructor.
FramesFactory - Class in org.orekit.frames
Factory for predefined reference frames.
FUTURE_INFINITY - Static variable in class org.orekit.time.AbsoluteDate
Dummy date at infinity in the future direction.

G

g(SpacecraftState) - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.AbstractDetector
Compute the value of the switching function.
g(double, double[]) - Method in class org.orekit.propagation.events.AdaptedEventDetector
g(SpacecraftState) - Method in class org.orekit.propagation.events.AlignmentDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.AltitudeDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.ApsideDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.DateDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.DihedralFieldOfViewDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.EclipseDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.ElevationDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in interface org.orekit.propagation.events.EventDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.EventShifter
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.NodeDetector
Compute the value of the switching function.
G0 - Static variable in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Reference gravity acceleration constant (m/s2).
GeodeticPoint - Class in org.orekit.bodies
Point location relative to a 2D body surface.
GeodeticPoint(double, double, double) - Constructor for class org.orekit.bodies.GeodeticPoint
Build a new instance.
get24HoursKp(AbsoluteDate) - Method in interface org.orekit.forces.drag.DTM2000InputParameters
Get the last 24H mean geomagnetic index.
getA() - Method in class org.orekit.orbits.CartesianOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.CircularOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.KeplerianOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.Orbit
Get the semi-major axis.
getA() - Method in class org.orekit.propagation.SpacecraftState
Get the semi-major axis.
getAbscissa(Vector3D) - Method in class org.orekit.utils.Line
Get the abscissa of a point with respect to the line.
getAbsorptionCoefficient() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Get the absorption coefficient.
getAbsorptionCoefficient() - Method in interface org.orekit.forces.radiation.RadiationSensitive
Get the absorption coefficient.
getAbsorptionCoefficient() - Method in class org.orekit.forces.SphericalSpacecraft
Get the absorption coefficient.
getAe() - Method in interface org.orekit.forces.gravity.potential.PotentialCoefficientsProvider
Get the value of the central body reference radius.
getAe() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the value of the central body reference radius.
getAlignAngle() - Method in class org.orekit.propagation.events.AlignmentDetector
Get the alignment angle (rad).
getAlphaE() - Method in class org.orekit.orbits.CircularOrbit
Get the eccentric longitude argument.
getAlphaM() - Method in class org.orekit.orbits.CircularOrbit
Get the mean longitude argument.
getAlphaV() - Method in class org.orekit.orbits.CircularOrbit
Get the true longitude argument.
getAltitude() - Method in class org.orekit.bodies.GeodeticPoint
Get the altitude.
getAltitude() - Method in class org.orekit.propagation.events.AltitudeDetector
Get the threshold altitude value.
getAp(AbsoluteDate) - Method in interface org.orekit.forces.drag.JB2006InputParameters
Get the Geomagnetic planetary 3-hour index Ap.
getArea() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft.Facet
Get facet area.
getAstronomicalUnit() - Static method in class org.orekit.bodies.JPLEphemeridesLoader
Deprecated. as of 4.2, replaced by the non-static method JPLEphemeridesLoader.getLoadedAstronomicalUnit()
getAttitude(Orbit) - Method in interface org.orekit.attitudes.AttitudeLaw
Compute the attitude corresponding to an orbital state.
getAttitude(Orbit) - Method in class org.orekit.attitudes.CelestialBodyPointed
Compute the attitude corresponding to an orbital state.
getAttitude(Orbit) - Method in class org.orekit.attitudes.FixedRate
Compute the attitude corresponding to an orbital state.
getAttitude(Orbit) - Method in class org.orekit.attitudes.GroundPointing
Compute the attitude corresponding to an orbital state.
getAttitude(Orbit) - Method in class org.orekit.attitudes.GroundPointingWrapper
Compute the attitude corresponding to an orbital state.
getAttitude(Orbit) - Method in class org.orekit.attitudes.InertialLaw
Compute the attitude corresponding to an orbital state.
getAttitude(Orbit) - Method in class org.orekit.attitudes.LofOffset
Compute the attitude corresponding to an orbital state.
getAttitude(Orbit) - Method in class org.orekit.attitudes.LofOffsetPointing
Compute the attitude corresponding to an orbital state.
getAttitude(Orbit) - Method in class org.orekit.attitudes.SpinStabilized
Compute the attitude corresponding to an orbital state.
getAttitude() - Method in class org.orekit.propagation.SpacecraftState
Get the attitude.
getAvailableSatelliteNumbers() - Method in class org.orekit.tle.TLESeries
Get the available satellite numbers.
getAxis1() - Method in class org.orekit.propagation.events.DihedralFieldOfViewDetector
Get the direction of fov 1st dihedral axis.
getAxis2() - Method in class org.orekit.propagation.events.DihedralFieldOfViewDetector
Get the direction of fov 2nd dihedral axis.
getAzimuth(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame
Get the azimuth of a point with regards to the topocentric frame center point.
getBaseState(Orbit) - Method in class org.orekit.attitudes.GroundPointingWrapper
Compute the base system state at given date, without compensation.
getBody(String) - Static method in class org.orekit.bodies.CelestialBodyFactory
Get a celestial body.
getBodyFrame() - Method in class org.orekit.attitudes.GroundPointing
Get the body frame.
getBodyFrame() - Method in interface org.orekit.bodies.BodyShape
Get body frame related to body shape.
getBodyFrame() - Method in class org.orekit.bodies.OneAxisEllipsoid
Get the body frame related to body shape.
getBodyShape() - Method in class org.orekit.propagation.events.AltitudeDetector
Get the body shape.
getBStar() - Method in class org.orekit.tle.TLE
Get the ballistic coefficient.
getC(int, int, boolean) - Method in interface org.orekit.forces.gravity.potential.PotentialCoefficientsProvider
Get the tesseral-sectorial and zonal coefficients.
getC(int, int, boolean) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the tesseral-sectorial and zonal coefficients.
getCalendarWeek() - Method in class org.orekit.time.DateComponents
Get the calendar week number.
getCalls() - Method in class org.orekit.propagation.numerical.NumericalPropagator
Get the number of calls to the differential equations computation method.
getCenter() - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector
Get the direction of fov center.
getCenter() - Method in class org.orekit.propagation.events.DihedralFieldOfViewDetector
Get the direction of fov center.
getCircularEx() - Method in class org.orekit.orbits.CircularOrbit
Get the first component of the circular eccentricity vector.
getCircularEy() - Method in class org.orekit.orbits.CircularOrbit
Get the second component of the circular eccentricity vector.
getCIRF2000() - Static method in class org.orekit.frames.Frame
Deprecated. as of 4.1, replaced by FramesFactory.getCIRF2000()
getCIRF2000() - Static method in class org.orekit.frames.FramesFactory
Get the CIRF2000 reference frame.
getClassification() - Method in class org.orekit.tle.TLE
Get the classification.
getClosestTLE(AbsoluteDate) - Method in class org.orekit.tle.TLESeries
Get the closest TLE to the selected date.
getCompensation(Orbit, Attitude) - Method in class org.orekit.attitudes.GroundPointingWrapper
Compute the compensation rotation at given date.
getCompensation(Orbit, Attitude) - Method in class org.orekit.attitudes.YawCompensation
Compute the compensation rotation at given date.
getCompensation(Orbit, Attitude) - Method in class org.orekit.attitudes.YawSteering
Compute the compensation rotation at given date.
getComponents(TimeScale) - Method in class org.orekit.time.AbsoluteDate
Split the instance into date/time components.
getConstant(String) - Static method in class org.orekit.bodies.JPLEphemeridesLoader
Deprecated. as of 4.2, replaced by the non-static method JPLEphemeridesLoader.getLoadedConstant(String)
getCurrentDate() - Method in class org.orekit.propagation.sampling.AdaptedStepHandler
Get the current grid date.
getCurrentDate() - Method in class org.orekit.propagation.sampling.BasicStepInterpolator
Get the current grid date.
getCurrentDate() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
Get the current grid date.
getD() - Method in class org.orekit.data.BodiesElements
Get the mean elongation of the Moon from the Sun.
getDate() - Method in class org.orekit.attitudes.Attitude
Get the date of attitude parameters.
getDate() - Method in class org.orekit.frames.EOPEntry
Get the date.
getDate() - Method in class org.orekit.orbits.Orbit
Get the date of orbital parameters.
getDate() - Method in class org.orekit.propagation.events.DateDetector
Get the target date.
getDate() - Method in class org.orekit.propagation.SpacecraftState
Get the date.
getDate() - Method in class org.orekit.time.AbsoluteDate
Get the date.
getDate() - Method in class org.orekit.time.DateTimeComponents
Get the date component.
getDate() - Method in interface org.orekit.time.TimeStamped
Get the date.
getDate() - Method in class org.orekit.tle.TLE
Get the TLE current date.
getDay() - Method in class org.orekit.time.DateComponents
Get the day.
getDayOfWeek() - Method in class org.orekit.time.DateComponents
Get the day of week.
getDayOfYear() - Method in class org.orekit.time.DateComponents
Get the day number in year.
getDdEps() - Method in class org.orekit.frames.EOP1980Entry
Get the correction for nutation in obliquity.
getDdeps() - Method in class org.orekit.frames.NutationCorrection
Get the δΔε1980 parameter.
getDdPsi() - Method in class org.orekit.frames.EOP1980Entry
Get the correction for nutation in longitude.
getDdpsi() - Method in class org.orekit.frames.NutationCorrection
Get the δΔψ1980 parameter.
getDecreasingTimeShift() - Method in class org.orekit.propagation.events.EventShifter
Get the decreasing events time shift.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in interface org.orekit.forces.drag.Atmosphere
Get the local density.
getDensity(int, double, double, double, double, double, double, double, double) - Method in class org.orekit.forces.drag.DTM2000
Get the local density with initial entries.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.DTM2000
Get the local density.
getDensity(double, double, double, double, double, double, double, double, double, double, double, double, double) - Method in class org.orekit.forces.drag.JB2006
Get the local density with initial entries.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.JB2006
Get the local density.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.SimpleExponentialAtmosphere
Get the local density.
getDirection() - Method in class org.orekit.utils.Line
Get the normalized direction vector.
getDragCoefficient() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Get the drag coefficient.
getDragCoefficient() - Method in interface org.orekit.forces.drag.DragSensitive
Get the drag coefficient.
getDragCoefficient() - Method in class org.orekit.forces.SphericalSpacecraft
Get the drag coefficient.
getDUT1(AbsoluteDate) - Method in class org.orekit.frames.TidalCorrection
Get the dUT1 value.
getE() - Method in class org.orekit.orbits.CartesianOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.CircularOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.KeplerianOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.Orbit
Get the eccentricity.
getE() - Method in class org.orekit.propagation.SpacecraftState
Get the eccentricity.
getE() - Method in class org.orekit.tle.TLE
Get the eccentricity.
getEarth() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Earth singleton body.
getEarth() - Static method in class org.orekit.bodies.SolarSystemBody
Deprecated. Get the Earth singleton body.
getEarthMoonBarycenter() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Earth-Moon barycenter singleton bodies pair.
getEarthMoonBarycenter() - Static method in class org.orekit.bodies.SolarSystemBody
Deprecated. Get the Earth-Moon barycenter singleton bodies pair.
getEarthMoonMassRatio() - Static method in class org.orekit.bodies.JPLEphemeridesLoader
Deprecated. as of 4.2, replaced by the non-static method JPLEphemeridesLoader.getLoadedEarthMoonMassRatio()
getEast() - Method in class org.orekit.bodies.GeodeticPoint
Get the direction to the east of point, expressed in parent shape frame.
getEast() - Method in class org.orekit.frames.TopocentricFrame
Get the east direction of topocentric frame, expressed in parent shape frame.
getEccentricAnomaly() - Method in class org.orekit.orbits.KeplerianOrbit
Get the eccentric anomaly.
getElementNumber() - Method in class org.orekit.tle.TLE
Get the element number.
getElevation(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame
Get the elevation of a point with regards to the local point.
getElevation() - Method in class org.orekit.propagation.events.ElevationDetector
Get the threshold elevation value (°).
getEME2000() - Static method in class org.orekit.frames.Frame
Deprecated. as of 4.1, replaced by FramesFactory.getEME2000()
getEME2000() - Static method in class org.orekit.frames.FramesFactory
Get the unique EME2000 frame.
getEndDate() - Method in class org.orekit.frames.AbstractEOPHistory
Get the date of the last available Earth Orientation Parameters.
getEndDate() - Method in interface org.orekit.frames.EOPHistory
Get the date of the last available Earth Orientation Parameters.
getEOP1980History() - Static method in class org.orekit.frames.FramesFactory
Get Earth Orientation Parameters history (IAU1980) data.
getEOP2000History() - Static method in class org.orekit.frames.FramesFactory
Get Earth Orientation Parameters history (IAU2000) data.
getEphemerisType() - Method in class org.orekit.tle.TLE
Get the type of ephemeris.
getEquatorialRadius() - Method in class org.orekit.bodies.OneAxisEllipsoid
Get the equatorial radius of the body.
getEquinoctialEx() - Method in class org.orekit.orbits.CartesianOrbit
Get the first component of the eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.CircularOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the first component of the eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.KeplerianOrbit
Get the first component of the eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.Orbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.propagation.SpacecraftState
Get the first component of the eccentricity vector (as per equinoctial parameters).
getEquinoctialEy() - Method in class org.orekit.orbits.CartesianOrbit
Get the second component of the eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.CircularOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the second component of the eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.KeplerianOrbit
Get the second component of the eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.Orbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.propagation.SpacecraftState
Get the second component of the eccentricity vector (as per equinoctial parameters).
getEventsDetectors() - Method in class org.orekit.forces.drag.DragForce
There are no discrete events for this model.
getEventsDetectors() - Method in interface org.orekit.forces.ForceModel
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.CunninghamAttractionModel
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.DrozinerAttractionModel
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.ThirdBodyAttraction
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.AbstractPropagator
Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.events.CombinedEventsDetectorsManager
Get all the events detectors that have been added to the manager.
getEventsDetectors() - Method in class org.orekit.propagation.numerical.NumericalPropagator
Get all the events detectors that have been added.
getEventsDetectors() - Method in interface org.orekit.propagation.Propagator
Get all the events detectors that have been added.
getEventTime() - Method in class org.orekit.propagation.events.CombinedEventsDetectorsManager
Get the occurrence time of the first event triggered in the last evaluated step.
getExosphericTemp() - Method in class org.orekit.forces.drag.JB2006
Get the exospheric temperature above input position.
getF() - Method in class org.orekit.data.BodiesElements
Get L - Ω where L is the mean longitude of the Moon.
getF10(AbsoluteDate) - Method in interface org.orekit.forces.drag.JB2006InputParameters
Get the value of the instantaneous solar flux index (1e-22*Watt/(m2*Hertz)).
getF10B(AbsoluteDate) - Method in interface org.orekit.forces.drag.JB2006InputParameters
Get the value of the mean solar flux.
getFirst() - Method in class org.orekit.tle.TLESeries
Get the first TLE.
getFirstDate() - Method in class org.orekit.tle.TLESeries
Get the start date of the series.
getFirstKnownLeapSecond() - Method in class org.orekit.time.UTCScale
Get the date of the first known leap second.
getFrame() - Method in class org.orekit.bodies.AbstractCelestialBody
Get an inertially oriented body-centered frame.
getFrame() - Method in interface org.orekit.bodies.CelestialBody
Get an inertially oriented body-centered frame.
getFrame() - Method in class org.orekit.orbits.Orbit
Get the frame in which the orbital parameters are defined.
getFrame() - Method in class org.orekit.propagation.events.NodeDetector
Get the frame in which the equator is defined.
getFrame() - Method in class org.orekit.propagation.SpacecraftState
Get the inertial frame.
getGCRF() - Static method in class org.orekit.frames.FramesFactory
Get the unique GCRF frame.
getGeneratedEphemeris() - Method in class org.orekit.propagation.AbstractPropagator
Get the ephemeris generated during propagation.
getGeneratedEphemeris() - Method in class org.orekit.propagation.numerical.NumericalPropagator
Get the ephemeris generated during propagation.
getGeneratedEphemeris() - Method in interface org.orekit.propagation.Propagator
Get the ephemeris generated during propagation.
getGM() - Method in class org.orekit.bodies.AbstractCelestialBody
Get the attraction coefficient of the body.
getGM() - Method in interface org.orekit.bodies.CelestialBody
Get the attraction coefficient of the body.
getGPS() - Static method in class org.orekit.time.TimeScalesFactory
Get the Global Positioning System scale.
getGravitationalCoefficient(JPLEphemeridesLoader.EphemerisType) - Static method in class org.orekit.bodies.JPLEphemeridesLoader
Deprecated. as of 4.2, replaced by the non-static method JPLEphemeridesLoader.getLoadedGravitationalCoefficient(EphemerisType)
getGroundPointingLaw() - Method in class org.orekit.attitudes.GroundPointingWrapper
Get the attitude rotation.
getHalfAperture() - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector
Get fov half aperture angle.
getHalfAperture1() - Method in class org.orekit.propagation.events.DihedralFieldOfViewDetector
Get the half aperture angle of fov 1st dihedra.
getHalfAperture2() - Method in class org.orekit.propagation.events.DihedralFieldOfViewDetector
Get the half aperture angle of fov 2nd dihedra.
getHour() - Method in class org.orekit.time.TimeComponents
Get the hour number.
getHx() - Method in class org.orekit.orbits.CartesianOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.CircularOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.KeplerianOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.Orbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.propagation.SpacecraftState
Get the first component of the inclination vector (as per equinoctial parameters).
getHy() - Method in class org.orekit.orbits.CartesianOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.CircularOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.KeplerianOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.Orbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.propagation.SpacecraftState
Get the second component of the inclination vector (as per equinoctial parameters).
getI() - Method in class org.orekit.orbits.CartesianOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.CircularOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.KeplerianOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.Orbit
Get the inclination.
getI() - Method in class org.orekit.propagation.SpacecraftState
Get the inclination.
getI() - Method in class org.orekit.tle.TLE
Get the inclination.
getIncreasingTimeShift() - Method in class org.orekit.propagation.events.EventShifter
Get the increasing events time shift.
getInitialState() - Method in class org.orekit.propagation.AbstractPropagator
Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.analytical.KeplerianPropagator
Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.numerical.NumericalPropagator
Get the propagator initial state.
getInitialState() - Method in interface org.orekit.propagation.Propagator
Get the propagator initial state.
getInstance() - Static method in class org.orekit.data.DataProvidersManager
Get the unique instance.
getInstance() - Static method in class org.orekit.time.GPSScale
Deprecated. since 4.1 replaced by TimeScalesFactory.getGPS()
getInstance() - Static method in class org.orekit.time.TAIScale
Deprecated. since 4.1 replaced by TimeScalesFactory.getTAI()
getInstance() - Static method in class org.orekit.time.TCGScale
Deprecated. since 4.1 replaced by TimeScalesFactory.getTCG()
getInstance() - Static method in class org.orekit.time.TTScale
Deprecated. since 4.1 replaced by TimeScalesFactory.getTT()
getInstance() - Static method in class org.orekit.time.UTCScale
Deprecated. since 4.1 replaced by TimeScalesFactory.getUTC()
getInstantFlux(AbsoluteDate) - Method in interface org.orekit.forces.drag.DTM2000InputParameters
Get the value of the instantaneous solar flux.
getInterpolatedDate() - Method in class org.orekit.propagation.sampling.AdaptedStepHandler
Get the interpolated date.
getInterpolatedDate() - Method in class org.orekit.propagation.sampling.BasicStepInterpolator
Get the interpolated date.
getInterpolatedDate() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
Get the interpolated date.
getInterpolatedState() - Method in class org.orekit.propagation.sampling.AdaptedStepHandler
Get the interpolated state.
getInterpolatedState() - Method in class org.orekit.propagation.sampling.BasicStepInterpolator
Get the interpolated state.
getInterpolatedState() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
Get the interpolated state.
getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in interface org.orekit.bodies.BodyShape
Get the intersection point of a line with the surface of the body.
getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.bodies.OneAxisEllipsoid
Get the intersection point of a line with the surface of the body.
getInverse() - Method in class org.orekit.frames.Transform
Get the inverse transform of the instance.
getITRF2005() - Static method in class org.orekit.frames.Frame
Deprecated. as of 4.1, replaced by FramesFactory.getITRF2005()
getITRF2005() - Static method in class org.orekit.frames.FramesFactory
Get the ITRF2005 reference frame, ignoring tidal effects.
getITRF2005(boolean) - Static method in class org.orekit.frames.FramesFactory
Get the ITRF2005 reference frame.
getJ(boolean, int) - Method in interface org.orekit.forces.gravity.potential.PotentialCoefficientsProvider
Get the zonal coefficients.
getJ(boolean, int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the zonal coefficients.
getJ2000() - Static method in class org.orekit.frames.Frame
Deprecated. as of 4.0, replaced by FramesFactory.getEME2000()
getJ2000Day() - Method in class org.orekit.time.DateComponents
Get the day number with respect to J2000 epoch.
getJupiter() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Jupiter singleton body.
getJupiter() - Static method in class org.orekit.bodies.SolarSystemBody
Deprecated. Get the Jupiter singleton body.
getKeplerianMeanMotion() - Method in class org.orekit.orbits.Orbit
Get the keplerian mean motion.
getKeplerianMeanMotion() - Method in class org.orekit.propagation.SpacecraftState
Get the keplerian mean motion.
getKeplerianPeriod() - Method in class org.orekit.orbits.Orbit
Get the keplerian period.
getKeplerianPeriod() - Method in class org.orekit.propagation.SpacecraftState
Get the keplerian period.
getL() - Method in class org.orekit.data.BodiesElements
Get the mean anomaly of the Moon.
getLast() - Method in class org.orekit.tle.TLESeries
Get the last TLE.
getLastDate() - Method in class org.orekit.tle.TLESeries
Get the last date of the series.
getLastKnownLeapSecond() - Method in class org.orekit.time.UTCScale
Get the date of the last known leap second.
getLatitude() - Method in class org.orekit.bodies.GeodeticPoint
Get the latitude.
getLaunchNumber() - Method in class org.orekit.tle.TLE
Get the launch number.
getLaunchPiece() - Method in class org.orekit.tle.TLE
Get the launch piece.
getLaunchYear() - Method in class org.orekit.tle.TLE
Get the launch year.
getLE() - Method in class org.orekit.data.BodiesElements
Get the mean Earth longitude.
getLE() - Method in class org.orekit.orbits.CartesianOrbit
Get the eccentric latitude argument.
getLE() - Method in class org.orekit.orbits.CircularOrbit
Get the eccentric latitude argument.
getLE() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the eccentric latitude argument.
getLE() - Method in class org.orekit.orbits.KeplerianOrbit
Get the eccentric latitude argument.
getLE() - Method in class org.orekit.orbits.Orbit
Get the eccentric latitude argument.
getLE() - Method in class org.orekit.propagation.SpacecraftState
Get the eccentric latitude argument (as per equinoctial parameters).
getLeap(AbsoluteDate) - Method in class org.orekit.time.UTCScale
Get the value of the previous leap.
getLightningRatio(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Get the lightning ratio ([0-1]).
getLine1() - Method in class org.orekit.tle.TLE
Get the first line.
getLine2() - Method in class org.orekit.tle.TLE
Get the second line.
getLJu() - Method in class org.orekit.data.BodiesElements
Get the mean Jupiter longitude.
getLM() - Method in class org.orekit.orbits.CartesianOrbit
Get the mean latitude argument.
getLM() - Method in class org.orekit.orbits.CircularOrbit
Get the mean latitude argument.
getLM() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the mean latitude argument.
getLM() - Method in class org.orekit.orbits.KeplerianOrbit
Get the mean latitude argument.
getLM() - Method in class org.orekit.orbits.Orbit
Get the mean latitude argument.
getLM() - Method in class org.orekit.propagation.SpacecraftState
Get the mean latitude argument (as per equinoctial parameters).
getLMa() - Method in class org.orekit.data.BodiesElements
Get the mean Mars longitude.
getLMe() - Method in class org.orekit.data.BodiesElements
Get the mean Mercury longitude.
getLNe() - Method in class org.orekit.data.BodiesElements
Get the mean Neptune longitude.
getLoadedAstronomicalUnit() - Method in class org.orekit.bodies.JPLEphemeridesLoader
Get astronomical unit.
getLoadedConstant(String) - Method in class org.orekit.bodies.JPLEphemeridesLoader
Get a constant defined in the ephemerides headers.
getLoadedEarthMoonMassRatio() - Method in class org.orekit.bodies.JPLEphemeridesLoader
Get Earth/Moon mass ratio.
getLoadedGravitationalCoefficient(JPLEphemeridesLoader.EphemerisType) - Method in class org.orekit.bodies.JPLEphemeridesLoader
Get the gravitational coefficient of a body.
getLocalizedMessage() - Method in exception org.orekit.errors.OrekitException
getLocalTemp() - Method in class org.orekit.forces.drag.JB2006
Get the temperature at input position.
getLOD(AbsoluteDate) - Method in class org.orekit.frames.AbstractEOPHistory
Get the LoD (Length of Day) value.
getLOD() - Method in class org.orekit.frames.EOPEntry
Get the LoD (Length of Day) value.
getLOD(AbsoluteDate) - Method in interface org.orekit.frames.EOPHistory
Get the LoD (Length of Day) value.
getLongitude() - Method in class org.orekit.bodies.GeodeticPoint
Get the longitude.
getLPrime() - Method in class org.orekit.data.BodiesElements
Get the mean anomaly of the Sun.
getLSa() - Method in class org.orekit.data.BodiesElements
Get the mean Saturn longitude.
getLUr() - Method in class org.orekit.data.BodiesElements
Get the mean Uranus longitude.
getLv() - Method in class org.orekit.orbits.CartesianOrbit
Get the true latitude argument.
getLv() - Method in class org.orekit.orbits.CircularOrbit
Get the true latitude argument.
getLv() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the true latitude argument.
getLv() - Method in class org.orekit.orbits.KeplerianOrbit
Get the true latitude argument.
getLv() - Method in class org.orekit.orbits.Orbit
Get the true latitude argument.
getLv() - Method in class org.orekit.propagation.SpacecraftState
Get the true latitude argument (as per equinoctial parameters).
getLVe() - Method in class org.orekit.data.BodiesElements
Get the mean Venus longitude.
getMam() - Method in class org.orekit.forces.drag.DTM2000
Get the local mean atomic mass.
getMars() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Mars singleton body.
getMars() - Static method in class org.orekit.bodies.SolarSystemBody
Deprecated. Get the Mars singleton body.
getMass() - Method in class org.orekit.propagation.SpacecraftState
Gets the current mass.
getMaxCheckInterval() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Get maximal time interval between switching function checks.
getMaxCheckInterval() - Method in class org.orekit.propagation.events.AbstractDetector
Get maximal time interval between switching function checks.
getMaxCheckInterval() - Method in interface org.orekit.propagation.events.EventDetector
Get maximal time interval between switching function checks.
getMaxChunksDuration() - Method in class org.orekit.bodies.JPLEphemeridesLoader
Get the maximal chunks duration.
getMaxDate() - Method in interface org.orekit.forces.drag.DTM2000InputParameters
Gets the available data range maximum date.
getMaxDate() - Method in interface org.orekit.forces.drag.JB2006InputParameters
Gets the available data range maximum date.
getMaxDate() - Method in interface org.orekit.propagation.BoundedPropagator
Get the last date of the range.
getMaxDate() - Method in class org.orekit.propagation.Ephemeris
Get the last date of the range.
getMaxIterationCount() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Get maximal number of iterations in the event time search.
getMaxIterationCount() - Method in class org.orekit.propagation.events.AbstractDetector
Get maximal number of iterations in the event time search.
getMaxIterationCount() - Method in interface org.orekit.propagation.events.EventDetector
Get maximal number of iterations in the event time search.
getMeanAnomaly() - Method in class org.orekit.orbits.KeplerianOrbit
Get the mean anomaly.
getMeanAnomaly() - Method in class org.orekit.tle.TLE
Get the mean anomaly.
getMeanFlux(AbsoluteDate) - Method in interface org.orekit.forces.drag.DTM2000InputParameters
Get the value of the mean solar flux.
getMeanMotion() - Method in class org.orekit.tle.TLE
Get the mean motion.
getMeanMotionFirstDerivative() - Method in class org.orekit.tle.TLE
Get the mean motion first derivative.
getMeanMotionSecondDerivative() - Method in class org.orekit.tle.TLE
Get the mean motion second derivative.
getMEME(boolean) - Static method in class org.orekit.frames.FramesFactory
Get the MEME reference frame.
getMercury() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Mercury singleton body.
getMercury() - Static method in class org.orekit.bodies.SolarSystemBody
Deprecated. Get the Mercury singleton body.
getMessage(Locale) - Method in exception org.orekit.errors.OrekitException
Gets the message in a specified locale.
getMessage() - Method in exception org.orekit.errors.OrekitException
getMinDate() - Method in interface org.orekit.forces.drag.DTM2000InputParameters
Gets the available data range minimum date.
getMinDate() - Method in interface org.orekit.forces.drag.JB2006InputParameters
Gets the available data range minimum date.
getMinDate() - Method in interface org.orekit.propagation.BoundedPropagator
Get the first date of the range.
getMinDate() - Method in class org.orekit.propagation.Ephemeris
Get the first date of the range.
getMinute() - Method in class org.orekit.time.TimeComponents
Get the minute number.
getMjd() - Method in class org.orekit.frames.EOPEntry
Get the entry date (modified julian day, 00h00 UTC scale).
getMJD() - Method in class org.orekit.time.DateComponents
Get the modified julian day.
getMode() - Method in class org.orekit.propagation.AbstractPropagator
Get the current operating mode of the propagator.
getMode() - Method in class org.orekit.propagation.numerical.NumericalPropagator
Get the current operating mode of the propagator.
getMode() - Method in interface org.orekit.propagation.Propagator
Get the current operating mode of the propagator.
getMomentum() - Method in class org.orekit.utils.PVCoordinates
Gets the momentum.
getMonth() - Method in class org.orekit.time.DateComponents
Get the month.
getMoon() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Moon singleton body.
getMoon() - Static method in class org.orekit.bodies.SolarSystemBody
Deprecated. Get the Moon singleton body.
getMu() - Method in interface org.orekit.forces.gravity.potential.PotentialCoefficientsProvider
Get the central body attraction coefficient.
getMu() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the central body attraction coefficient.
getMu() - Method in class org.orekit.orbits.Orbit
Get the central acceleration constant.
getMu() - Method in class org.orekit.propagation.numerical.NumericalPropagator
Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.propagation.SpacecraftState
Get the central attraction coefficient.
getN() - Method in class org.orekit.propagation.numerical.TimeDerivativesEquations
Get the second vector of the (t, n, w) local orbital frame.
getNadir() - Method in class org.orekit.bodies.GeodeticPoint
Get the direction below the point, expressed in parent shape frame.
getNadir() - Method in class org.orekit.frames.TopocentricFrame
Get the nadir direction of topocentric frame, expressed in parent shape frame.
getName() - Method in class org.orekit.frames.Frame
Get the name.
getName() - Method in class org.orekit.time.GPSScale
Get the name time scale.
getName() - Method in class org.orekit.time.TAIScale
Get the name time scale.
getName() - Method in class org.orekit.time.TCGScale
Get the name time scale.
getName() - Method in class org.orekit.time.TDBScale
Get the name time scale.
getName() - Method in interface org.orekit.time.TimeScale
Get the name time scale.
getName() - Method in class org.orekit.time.TTScale
Get the name time scale.
getName() - Method in class org.orekit.time.UTCScale
Get the name time scale.
getNeptune() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Neptune singleton body.
getNeptune() - Static method in class org.orekit.bodies.SolarSystemBody
Deprecated. Get the Neptune singleton body.
getNonRotatingLaw() - Method in class org.orekit.attitudes.SpinStabilized
Get the underlying non-rotating attitude law.
getNormal() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft.Facet
Get unit normal vector.
getNormal(SpacecraftState) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Get solar array normal in spacecraft frame.
getNorth() - Method in class org.orekit.bodies.GeodeticPoint
Get the direction to the north of point, expressed in parent shape frame.
getNorth() - Method in class org.orekit.frames.TopocentricFrame
Get the north direction of topocentric frame, expressed in parent shape frame.
getNutationCorrection(AbsoluteDate) - Method in class org.orekit.frames.EOP1980History
Get the correction to the nutation parameters.
getOcculted() - Method in class org.orekit.propagation.events.EclipseDetector
Get the occulted body.
getOccultedRadius() - Method in class org.orekit.propagation.events.EclipseDetector
Get the occulted body radius (m).
getOcculting() - Method in class org.orekit.propagation.events.EclipseDetector
Get the occulting body.
getOccultingRadius() - Method in class org.orekit.propagation.events.EclipseDetector
Get the occulting body radius (m).
getOmega() - Method in class org.orekit.data.BodiesElements
Get the mean longitude of the ascending node of the Moon.
getOrbit() - Method in class org.orekit.propagation.SpacecraftState
Gets the current orbit.
getOrigin() - Method in class org.orekit.utils.Line
Get the line point closest to the origin.
geTotaltEclipse() - Method in class org.orekit.propagation.events.EclipseDetector
Get the total eclipse detection flag.
getPa() - Method in class org.orekit.data.BodiesElements
Get the general accumulated precession in longitude.
getParameter(String) - Method in class org.orekit.forces.drag.DragForce
Get parameter value from its name.
getParameter(String) - Method in interface org.orekit.forces.Parameterizable
Get parameter value from its name.
getParameter(String) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Get parameter value from its name.
getParameterNames() - Method in class org.orekit.propagation.numerical.NumericalPropagatorWithJacobians
Get the parameters selected for jacobian processing.
getParametersNames() - Method in class org.orekit.forces.drag.DragForce
Get the names of the supported parameters for partial derivatives processing.
getParametersNames() - Method in interface org.orekit.forces.Parameterizable
Get the names of the supported parameters for partial derivatives processing.
getParametersNames() - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Get the names of the supported parameters for partial derivatives processing.
getParent() - Method in class org.orekit.frames.Frame
Get the parent frame.
getParentShape() - Method in class org.orekit.frames.TopocentricFrame
Get the body shape on which the local point is defined.
getPartialDensities(int) - Method in class org.orekit.forces.drag.DTM2000
Get the local partial density of the selected element.
getPEF(boolean) - Static method in class org.orekit.frames.FramesFactory
Get the PEF reference frame.
getPerigeeArgument() - Method in class org.orekit.orbits.KeplerianOrbit
Get the perigee argument.
getPerigeeArgument() - Method in class org.orekit.tle.TLE
Get the argument of perigee.
getPluto() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Pluto singleton body.
getPluto() - Static method in class org.orekit.bodies.SolarSystemBody
Deprecated. Get the Pluto singleton body.
getPoleCorrection(AbsoluteDate) - Method in class org.orekit.frames.EOP2000History
Get the pole IERS Reference Pole correction.
getPoleCorrection(AbsoluteDate) - Method in class org.orekit.frames.TidalCorrection
Get the pole IERS Reference Pole correction.
getPosition() - Method in class org.orekit.utils.PVCoordinates
Gets the position.
getPotentialProvider() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get the gravity field coefficients provider from the first supported file.
getPotentialProvider() - Method in class org.orekit.forces.gravity.potential.PotentialReaderFactory
Deprecated. Get the gravity field coefficients provider from the first supported file.
getPreviousDate() - Method in class org.orekit.propagation.sampling.AdaptedStepHandler
Get the previous grid date.
getPreviousDate() - Method in class org.orekit.propagation.sampling.BasicStepInterpolator
Get the previous grid date.
getPreviousDate() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
Get the previous grid date.
getPropagator() - Method in class org.orekit.frames.SpacecraftFrame
Get the underlying propagator.
getProviders() - Method in class org.orekit.data.DataProvidersManager
Get an unmodifiable view of the list of supported providers.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.bodies.AbstractCelestialBody
Get the PVCoordinates of the body in the selected frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.frames.SpacecraftFrame
Get the PVCoordinates of the spacecraft frame origin in the selected frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.frames.TopocentricFrame
Get the PVCoordinates of the topocentric frame origin in the selected frame.
getPVCoordinates(Frame) - Method in class org.orekit.orbits.Orbit
Get the PVCoordinates.
getPVCoordinates() - Method in class org.orekit.orbits.Orbit
Get the PVCoordinates in definition frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.AbstractPropagator
Get the PVCoordinates of the body in the selected frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.Ephemeris
Get the PVCoordinates of the body in the selected frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Get the PVCoordinates of the body in the selected frame.
getPVCoordinates() - Method in class org.orekit.propagation.SpacecraftState
Get the PVCoordinates in orbit definition frame.
getPVCoordinates(Frame) - Method in class org.orekit.propagation.SpacecraftState
Get the PVCoordinates in given output frame.
getPVCoordinates(AbsoluteDate) - Method in class org.orekit.tle.TLEPropagator
Get the extrapolated position and velocity from an initial TLE.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.tle.TLEPropagator
Get the PVCoordinates of the body in the selected frame.
getPVCoordinates(AbsoluteDate) - Method in class org.orekit.tle.TLESeries
Get the extrapolated position and velocity from an initial date.
getPVCoordinates(AbsoluteDate, Frame) - Method in interface org.orekit.utils.PVCoordinatesProvider
Get the PVCoordinates of the body in the selected frame.
getPVCoordinatesProvider() - Method in class org.orekit.propagation.events.AlignmentDetector
Get the body to align.
getPVTarget() - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector
Get the position/velocity provider of the target .
getPVTarget() - Method in class org.orekit.propagation.events.DihedralFieldOfViewDetector
Get the position/velocity provider of the target .
getQ() - Method in class org.orekit.propagation.numerical.TimeDerivativesEquations
Get the first vector of the (q, s, w) local orbital frame.
getRaan() - Method in class org.orekit.tle.TLE
Get Right Ascension of the Ascending node.
getRange(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame
Get the range of a point with regards to the topocentric frame center point.
getRangeRate(PVCoordinates, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame
Get the range rate of a point with regards to the topocentric frame center point.
getReferenceAttitude() - Method in class org.orekit.attitudes.FixedRate
Get the reference attitude.
getReferenceFrame() - Method in class org.orekit.attitudes.Attitude
Get the reference frame.
getReflectionCoefficient() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Get the specular reflection coefficient.
getReflectionCoefficient() - Method in interface org.orekit.forces.radiation.RadiationSensitive
Get the specular reflection coefficient.
getReflectionCoefficient() - Method in class org.orekit.forces.SphericalSpacecraft
Get the specular reflection coefficient.
getRevolutionNumberAtEpoch() - Method in class org.orekit.tle.TLE
Get the revolution number.
getRightAscensionOfAscendingNode() - Method in class org.orekit.orbits.CircularOrbit
Get the right ascension of the ascending node.
getRightAscensionOfAscendingNode() - Method in class org.orekit.orbits.KeplerianOrbit
Get the right ascension of the ascending node.
getRoot() - Static method in class org.orekit.frames.Frame
Get the unique root frame.
getRotation() - Method in class org.orekit.attitudes.Attitude
Get the attitude rotation.
getRotation() - Method in class org.orekit.frames.Transform
Get the underlying elementary rotation.
getRotationRate() - Method in class org.orekit.frames.Transform
Get the first time derivative of the rotation.
getS(int, int, boolean) - Method in interface org.orekit.forces.gravity.potential.PotentialCoefficientsProvider
Get tesseral-sectorial coefficients.
getS(int, int, boolean) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get tesseral-sectorial coefficients.
getS() - Method in class org.orekit.propagation.numerical.TimeDerivativesEquations
Get the second vector of the (q, s, w) local orbital frame.
getS10(AbsoluteDate) - Method in interface org.orekit.forces.drag.JB2006InputParameters
Get the EUV index (26-34 nm) scaled to F10.
getS10B(AbsoluteDate) - Method in interface org.orekit.forces.drag.JB2006InputParameters
Get the EUV 81-day averaged centered index.
getSatelliteNumber() - Method in class org.orekit.tle.TLE
Get the satellite id.
getSaturn() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Saturn singleton body.
getSaturn() - Static method in class org.orekit.bodies.SolarSystemBody
Deprecated. Get the Saturn singleton body.
getSecond() - Method in class org.orekit.time.TimeComponents
Get the seconds number.
getSecondsInDay() - Method in class org.orekit.time.TimeComponents
Get the second number within the day.
getSolarSystemBarycenter() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the solar system barycenter aggregated body.
getSolarSystemBarycenter() - Static method in class org.orekit.bodies.SolarSystemBody
Deprecated. Get the solar system barycenter aggregated body.
getSouth() - Method in class org.orekit.bodies.GeodeticPoint
Get the direction to the south of point, expressed in parent shape frame.
getSouth() - Method in class org.orekit.frames.TopocentricFrame
Get the south direction of topocentric frame, expressed in parent shape frame.
getSpin() - Method in class org.orekit.attitudes.Attitude
Get the satellite spin.
getStartDate() - Method in class org.orekit.frames.AbstractEOPHistory
Get the date of the first available Earth Orientation Parameters.
getStartDate() - Method in interface org.orekit.frames.EOPHistory
Get the date of the first available Earth Orientation Parameters.
getSun() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Sun singleton body.
getSun() - Static method in class org.orekit.bodies.SolarSystemBody
Deprecated. Get the Sun singleton body.
getSupportedNames() - Method in interface org.orekit.bodies.CelestialBodyLoader
Get the regular expression for supported PV coordinates files names.
getSupportedNames() - Method in class org.orekit.bodies.JPLEphemeridesLoader
Get the regular expression for supported PV coordinates files names.
getSupportedNames() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the regular expression for supported files names.
getSupportedNames() - Method in interface org.orekit.time.UTCTAILoader
Get the regular expression for supported UTC-TAI offsets files names.
getT() - Method in class org.orekit.forces.drag.DTM2000
Get the local temperature.
getT() - Method in class org.orekit.propagation.numerical.TimeDerivativesEquations
Get the first vector of the (t, n, w) local orbital frame.
getTAI() - Static method in class org.orekit.time.TimeScalesFactory
Get the International Atomic Time scale.
getTargetPoint(Orbit, Frame) - Method in class org.orekit.attitudes.BodyCenterPointing
Compute the target point in specified frame.
getTargetPoint(Orbit, Frame) - Method in class org.orekit.attitudes.GroundPointing
Compute the target point in specified frame.
getTargetPoint(Orbit, Frame) - Method in class org.orekit.attitudes.GroundPointingWrapper
Compute the target point in specified frame.
getTargetPoint(Orbit, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing
Compute the target point in specified frame.
getTargetPoint(Orbit, Frame) - Method in class org.orekit.attitudes.NadirPointing
Compute the target point in specified frame.
getTargetPoint(Orbit, Frame) - Method in class org.orekit.attitudes.TargetPointing
Compute the target point in specified frame.
getTargetPV(Orbit, Frame) - Method in class org.orekit.attitudes.BodyCenterPointing
Compute the target point position/velocity in specified frame.
getTargetPV(Orbit, Frame) - Method in class org.orekit.attitudes.GroundPointing
Compute the target point position/velocity in specified frame.
getTargetPV(Orbit, Frame) - Method in class org.orekit.attitudes.GroundPointingWrapper
Compute the target point position/velocity in specified frame.
getTargetPV(Orbit, Frame) - Method in class org.orekit.attitudes.TargetPointing
Compute the target point position/velocity in specified frame.
getTCG() - Static method in class org.orekit.time.TimeScalesFactory
Get the Geocentric Coordinate Time scale.
getTDB() - Static method in class org.orekit.time.TimeScalesFactory
Get the Barycentric Dynamic Time scale.
getTEME(boolean) - Static method in class org.orekit.frames.FramesFactory
Get the TEME reference frame.
getThreeHourlyKP(AbsoluteDate) - Method in interface org.orekit.forces.drag.DTM2000InputParameters
Get the value of the 3H geomagnetic index.
getThreshold() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Get the convergence threshold in the event time search.
getThreshold() - Method in class org.orekit.propagation.events.AbstractDetector
Get the convergence threshold in the event time search.
getThreshold() - Method in interface org.orekit.propagation.events.EventDetector
Get the convergence threshold in the event time search.
getTime() - Method in class org.orekit.time.DateTimeComponents
Get the time component.
getTinf() - Method in class org.orekit.forces.drag.DTM2000
Get the current exospheric temperature above input position.
getTIRF2000() - Static method in class org.orekit.frames.Frame
Deprecated. as of 4.1, replaced by FramesFactory.getTIRF2000()
getTIRF2000() - Static method in class org.orekit.frames.FramesFactory
Get the TIRF2000 reference frame, ignoring tidal effects.
getTIRF2000(boolean) - Static method in class org.orekit.frames.FramesFactory
Get the TIRF2000 reference frame.
getTopocentricFrame() - Method in class org.orekit.propagation.events.ElevationDetector
Get the topocentric frame.
getTransformTo(Frame, AbsoluteDate) - Method in class org.orekit.frames.Frame
Get the transform from the instance to another frame.
getTranslation() - Method in class org.orekit.frames.Transform
Get the underlying elementary translation.
getTrueAnomaly() - Method in class org.orekit.orbits.KeplerianOrbit
Get the true anomaly.
getTT() - Static method in class org.orekit.time.TimeScalesFactory
Get the Terrestrial Time scale.
getUranus() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Uranus singleton body.
getUranus() - Static method in class org.orekit.bodies.SolarSystemBody
Deprecated. Get the Uranus singleton body.
getUT1MinusUTC(AbsoluteDate) - Method in class org.orekit.frames.AbstractEOPHistory
Get the UT1-UTC value.
getUT1MinusUTC() - Method in class org.orekit.frames.EOPEntry
Get the UT1-UTC value.
getUT1MinusUTC(AbsoluteDate) - Method in interface org.orekit.frames.EOPHistory
Get the UT1-UTC value.
getUTC() - Static method in class org.orekit.time.TimeScalesFactory
Get the Universal Time Coordinate scale.
getVeis1950() - Static method in class org.orekit.frames.Frame
Deprecated. as of 4.1, replaced by FramesFactory.getVeis1950()
getVeis1950() - Static method in class org.orekit.frames.FramesFactory
Get the VEIS 1950 reference frame.
getVelocity(AbsoluteDate, Vector3D, Frame) - Method in interface org.orekit.forces.drag.Atmosphere
Get the inertial velocity of atmosphere molecules.
getVelocity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.DTM2000
Get the inertial velocity of atmosphere molecules.
getVelocity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.JB2006
Get the inertial velocity of atmosphere molecules.
getVelocity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.SimpleExponentialAtmosphere
Get the inertial velocity of atmosphere molecules.
getVelocity() - Method in class org.orekit.frames.Transform
Get the first time derivative of the translation.
getVelocity() - Method in class org.orekit.utils.PVCoordinates
Gets the velocity.
getVenus() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Venus singleton body.
getVenus() - Static method in class org.orekit.bodies.SolarSystemBody
Deprecated. Get the Venus singleton body.
getW() - Method in class org.orekit.propagation.numerical.TimeDerivativesEquations
Get the third vector of both the (q, s, w) and (t, n, w) local orbital frames.
getWest() - Method in class org.orekit.bodies.GeodeticPoint
Get the direction to the west of point, expressed in parent shape frame.
getWest() - Method in class org.orekit.frames.TopocentricFrame
Get the west direction of topocentric frame, expressed in parent shape frame.
getX() - Method in class org.orekit.frames.EOP2000Entry
Get the X component of the pole motion.
getXM10(AbsoluteDate) - Method in interface org.orekit.forces.drag.JB2006InputParameters
Get the MG2 index scaled to F10.
getXM10B(AbsoluteDate) - Method in interface org.orekit.forces.drag.JB2006InputParameters
Get the MG2 81-day average centered index.
getXp() - Method in class org.orekit.frames.PoleCorrection
Get the xp parameter.
getY() - Method in class org.orekit.frames.EOP2000Entry
Get the Y component of the pole motion.
getYawAngle(Orbit) - Method in class org.orekit.attitudes.YawCompensation
Compute the yaw compensation angle at date.
getYear() - Method in class org.orekit.time.DateComponents
Get the year number.
getYp() - Method in class org.orekit.frames.PoleCorrection
Get the yp parameter.
getZenith() - Method in class org.orekit.bodies.GeodeticPoint
Get the direction above the point, expressed in parent shape frame.
getZenith() - Method in class org.orekit.frames.TopocentricFrame
Get the zenith direction of topocentric frame, expressed in parent shape frame.
GPS_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for GPS weeks: 1980-01-06T00:00:00 GPS time.
GPS_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for GPS weeks: 1980-01-06.
GPSScale - Class in org.orekit.time
GPS time scale.
GravityFieldFactory - Class in org.orekit.forces.gravity.potential
Factory used to read gravity field files in several supported formats.
GRGS_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory
Default regular expression for GRGS files.
GRGSFormatReader - Class in org.orekit.forces.gravity.potential
Reader for the GRGS gravity field format.
GRGSFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.GRGSFormatReader
Simple constructor.
GRIM5C1_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants
Earth angular velocity from GRIM5C1 model: 7.292115e-5 rad/s.
GRIM5C1_EARTH_C20 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized second zonal coefficient from GRIM5C1 model: -1.082626110612609e-3.
GRIM5C1_EARTH_C30 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized third zonal coefficient from GRIM5C1 model: 2.536150841690056e-6.
GRIM5C1_EARTH_C40 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized fourth zonal coefficient from GRIM5C1 model: 1.61936352497151e-6.
GRIM5C1_EARTH_C50 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized fifth zonal coefficient from GRIM5C1 model: 2.231013736607540e-7.
GRIM5C1_EARTH_C60 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized sixth zonal coefficient from GRIM5C1 model: -5.402895357302363e-7.
GRIM5C1_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth equatorial radius from GRIM5C1 model: 6378136.46 m.
GRIM5C1_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants
Earth flattening from GRIM5C1 model: 1.0 / 298.25765.
GRIM5C1_EARTH_MU - Static variable in interface org.orekit.utils.Constants
Earth gravitational constant from GRIM5C1 model: 3.986004415 m3/s2.
GroundPointing - Class in org.orekit.attitudes
This class handles ground pointing attitude laws.
GroundPointing(Frame) - Constructor for class org.orekit.attitudes.GroundPointing
Default constructor.
GroundPointingWrapper - Class in org.orekit.attitudes
This class leverages common parts for compensation modes around ground pointing attitudes.
GroundPointingWrapper(GroundPointing) - Constructor for class org.orekit.attitudes.GroundPointingWrapper
Creates a new instance.
GRS80_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants
Earth angular velocity from GRS80 model: 7.292115e-5 rad/s.
GRS80_EARTH_C20 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized second zonal coefficient from GRS80 model: -1.08263e-3.
GRS80_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth equatorial radius from GRS80 model: 6378137.0 m.
GRS80_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants
Earth flattening from GRS80 model: 1.0 / 298.257222101.
GRS80_EARTH_MU - Static variable in interface org.orekit.utils.Constants
Earth gravitational constant from GRS80 model: 3.986005e14 m3/s2.
GZIP_FILE_PATTERN - Static variable in interface org.orekit.data.DataProvider
Pattern for name of gzip files.

H

H00 - Static variable in class org.orekit.time.TimeComponents
Constant for commonly used hour 00:00:00.
H12 - Static variable in class org.orekit.time.TimeComponents
Constant for commonly used hour 12:00:00.
handleStep(StepInterpolator, boolean) - Method in class org.orekit.propagation.sampling.AdaptedStepHandler
handleStep(SpacecraftState, boolean) - Method in interface org.orekit.propagation.sampling.OrekitFixedStepHandler
Handle the current step.
handleStep(OrekitStepInterpolator, boolean) - Method in interface org.orekit.propagation.sampling.OrekitStepHandler
Handle the current step.
handleStep(OrekitStepInterpolator, boolean) - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer
Handle the last accepted step.
hashCode() - Method in class org.orekit.time.AbsoluteDate
Get a hashcode for this date.
hashCode() - Method in class org.orekit.time.DateComponents
hashCode() - Method in class org.orekit.time.DateTimeComponents
hashCode() - Method in class org.orekit.time.TimeComponents
HELIUM - Static variable in class org.orekit.forces.drag.DTM2000
Identifier for helium.
HYDROGEN - Static variable in class org.orekit.forces.drag.DTM2000
Identifier for hydrogen.

I

i - Variable in class org.orekit.tle.TLEPropagator
final inclination.
ICGEM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory
Default regular expression for ICGEM files.
ICGEMFormatReader - Class in org.orekit.forces.gravity.potential
Reader for the ICGEM gravity field format.
ICGEMFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.ICGEMFormatReader
Simple constructor.
IDENTITY - Static variable in class org.orekit.frames.Transform
Identity transform.
ImpulseManeuver - Class in org.orekit.forces.maneuvers
Impulse maneuver model.
ImpulseManeuver(EventDetector, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.ImpulseManeuver
Build a new instance.
InertialLaw - Class in org.orekit.attitudes
This class handles an inertial attitude law.
InertialLaw(Rotation) - Constructor for class org.orekit.attitudes.InertialLaw
Creates new instance.
initDerivatives(double[], EquinoctialOrbit) - Method in class org.orekit.propagation.numerical.TimeDerivativesEquations
Initialize all derivatives to zero.
initDerivativesWithJacobians(double[], double[][], double[][], EquinoctialOrbit) - Method in class org.orekit.propagation.numerical.TimeDerivativesEquationsWithJacobians
Initialize all derivatives and jacobians to zero.
initialize(AbsoluteDate, Frame, double, AttitudeLaw) - Method in interface org.orekit.propagation.numerical.ModeHandler
Initialize the mode handler.
initialize(AbsoluteDate, Frame, double, AttitudeLaw) - Method in class org.orekit.propagation.sampling.AdaptedStepHandler
Initialize the mode handler.
initialState - Variable in class org.orekit.propagation.numerical.NumericalPropagator
Initial state to propagate.
insideLeap(AbsoluteDate) - Method in class org.orekit.time.UTCScale
Check if date is within a leap second introduction.
integrator - Variable in class org.orekit.propagation.numerical.NumericalPropagator
Integrator selected by the user for the orbital extrapolation process.
isChildOf(Frame) - Method in class org.orekit.frames.Frame
Determine if a Frame is a child of another one.
isFormatOK(String, String) - Static method in class org.orekit.tle.TLE
Check the lines format validity.
isForward() - Method in class org.orekit.propagation.sampling.AdaptedStepHandler
Check is integration direction is forward in date.
isForward() - Method in class org.orekit.propagation.sampling.BasicStepInterpolator
Check is integration direction is forward in date.
isForward() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
Check is integration direction is forward in date.
isQuasiInertial() - Method in class org.orekit.frames.Frame
Check if the frame is quasi-inertial.
isSupported(Class<? extends DataProvider>) - Method in class org.orekit.data.DataProvidersManager
Check if some type of provider is supported.
iterator() - Method in class org.orekit.frames.AbstractEOPHistory

J

J2000_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
J2000.0 Reference epoch: 2000-01-01T12:00:00 Terrestrial Time (not UTC).
J2000_EPOCH - Static variable in class org.orekit.time.DateComponents
J2000.0 Reference epoch: 2000-01-01.
JAVA_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Java Reference epoch: 1970-01-01T00:00:00 TT.
JAVA_EPOCH - Static variable in class org.orekit.time.DateComponents
Java Reference epoch: 1970-01-01.
JB2006 - Class in org.orekit.forces.drag
This is the realization of the Jacchia-Bowman 2006 atmospheric model.
JB2006(JB2006InputParameters, PVCoordinatesProvider, BodyShape, Frame) - Constructor for class org.orekit.forces.drag.JB2006
Constructor with space environment information for internal computation.
JB2006InputParameters - Interface in org.orekit.forces.drag
Interface for solar activity and magnetic activity data.
JPL_SSD_ASTRONOMICAL_UNIT - Static variable in interface org.orekit.utils.Constants
Astronomical Unit: 149597870691 m.
JPL_SSD_EARTH_GM - Static variable in interface org.orekit.utils.Constants
Earth attraction coefficient (m3/s2).
JPL_SSD_EARTH_MOON_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Earth/Moon mass ratio: 81.30059.
JPL_SSD_EARTH_PLUS_MOON_GM - Static variable in interface org.orekit.utils.Constants
Sun/(Earth + Moon) attraction coefficient (m3/s2).
JPL_SSD_GAUSSIAN_GRAVITATIONAL_CONSTANT - Static variable in interface org.orekit.utils.Constants
Gaussian gravitational constant: 0.01720209895 √(AU3/d2).
JPL_SSD_JUPITER_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants
Sun/(Jupiter system) ttraction coefficient (m3/s2).
JPL_SSD_MARS_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants
Sun/(Mars system) attraction coefficient (m3/s2).
JPL_SSD_MERCURY_GM - Static variable in interface org.orekit.utils.Constants
Sun/Mercury attraction coefficient (m3/s2).
JPL_SSD_MOON_GM - Static variable in interface org.orekit.utils.Constants
Moon attraction coefficient (m3/s2).
JPL_SSD_NEPTUNE_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants
Sun/(Neptune system) attraction coefficient (m3/s2).
JPL_SSD_PLUTO_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants
Sun/(Pluto system) ttraction coefficient (m3/s2).
JPL_SSD_SATURN_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants
Sun/(Saturn system) attraction coefficient (m3/s2).
JPL_SSD_SUN_EARTH_PLUS_MOON_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/(Earth + Moon) mass ratio: 328900.56.
JPL_SSD_SUN_GM - Static variable in interface org.orekit.utils.Constants
Sun attraction coefficient (m3/s2).
JPL_SSD_SUN_JUPITER_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/(Jupiter system) mass ratio: 1047.3486.
JPL_SSD_SUN_MARS_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/(Mars system) mass ratio: 3098708.0.
JPL_SSD_SUN_MERCURY_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/Mercury mass ratio: 6023600.
JPL_SSD_SUN_NEPTUNE_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/(Neptune system) mass ratio: 19412.24.
JPL_SSD_SUN_PLUTO_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/(Pluto system) mass ratio: 1.35e8.
JPL_SSD_SUN_SATURN_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/(Saturn system) mass ratio: 3497.898.
JPL_SSD_SUN_URANUS_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/(Uranus system) mass ratio: 22902.98.
JPL_SSD_SUN_VENUS_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/Venus mass ratio: 408523.71.
JPL_SSD_URANUS_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants
Sun/(Uranus system) attraction coefficient (m3/s2).
JPL_SSD_VENUS_GM - Static variable in interface org.orekit.utils.Constants
Sun/Venus attraction coefficient (m3/s2).
JPLEphemeridesLoader - Class in org.orekit.bodies
Loader for JPL ephemerides binary files (DE 405, DE 406).
JPLEphemeridesLoader(String, JPLEphemeridesLoader.EphemerisType, AbsoluteDate) - Constructor for class org.orekit.bodies.JPLEphemeridesLoader
Create a loader for JPL ephemerides binary files.
JPLEphemeridesLoader.EphemerisType - Enum in org.orekit.bodies
List of supported ephemerides types.
JULIAN_CENTURY - Static variable in interface org.orekit.utils.Constants
Duration of a julian century: 36525 Constants.JULIAN_DAY.
JULIAN_DAY - Static variable in interface org.orekit.utils.Constants
Duration of a mean solar day: 86400.0 s.
JULIAN_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for julian dates: -4712-01-01T12:00:00.
JULIAN_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for julian dates: -4712-01-01.
JULIAN_YEAR - Static variable in interface org.orekit.utils.Constants
Duration of a julian year: 365.25 Constants.JULIAN_DAY.
JUPITER - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Jupiter.

K

KeplerianOrbit - Class in org.orekit.orbits
This class handles traditional keplerian orbital parameters.
KeplerianOrbit(double, double, double, double, double, double, int, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.KeplerianOrbit
Creates a new instance.
KeplerianOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.KeplerianOrbit
Constructor from cartesian parameters.
KeplerianOrbit(Orbit) - Constructor for class org.orekit.orbits.KeplerianOrbit
Constructor from any kind of orbital parameters.
KeplerianPropagator - Class in org.orekit.propagation.analytical
Simple keplerian orbit propagator.
KeplerianPropagator(Orbit) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator
Build a propagator from orbit only.
KeplerianPropagator(Orbit, double) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator
Build a propagator from orbit and central attraction coefficient μ.
KeplerianPropagator(Orbit, AttitudeLaw) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator
Build a propagator from orbit and attitude law.
KeplerianPropagator(Orbit, AttitudeLaw, double) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator
Build a propagator from orbit, attitude law and central attraction coefficient μ.
KeplerianPropagator(Orbit, AttitudeLaw, double, double) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator
Build propagator from orbit, attitude law, central attraction coefficient μ and mass.

L

Line - Class in org.orekit.utils
The class represent lines in a three dimensional space.
Line(Vector3D, Vector3D) - Constructor for class org.orekit.utils.Line
Build a line from a point and a direction.
loadCelestialBody(String) - Method in interface org.orekit.bodies.CelestialBodyLoader
Load celestial body.
loadCelestialBody(String) - Method in class org.orekit.bodies.JPLEphemeridesLoader
Load celestial body.
loadData(InputStream, String) - Method in class org.orekit.bodies.JPLEphemeridesLoader
Load data from a stream.
loadData(InputStream, String) - Method in interface org.orekit.data.DataLoader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.EGMFormatReader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.GRGSFormatReader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.ICGEMFormatReader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.SHMFormatReader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.tle.TLESeries
Load data from a stream.
loadTimeSteps() - Method in interface org.orekit.time.UTCTAILoader
Load UTC-TAI offsets entries.
loadTLEData() - Method in class org.orekit.tle.TLESeries
Load TLE data for a specified object.
loadTLEData(int) - Method in class org.orekit.tle.TLESeries
Load TLE data for a specified object.
loadTLEData(int, int, String) - Method in class org.orekit.tle.TLESeries
Load TLE data for a specified object.
LocalOrbitalFrame - Class in org.orekit.frames
Class for frames moving with an orbiting satellite.
LocalOrbitalFrame(Frame, LocalOrbitalFrame.LOFType, PVCoordinatesProvider, String) - Constructor for class org.orekit.frames.LocalOrbitalFrame
Build a new instance.
LocalOrbitalFrame.LOFType - Enum in org.orekit.frames
List of supported frames types.
LOF_ALIGNED - Static variable in class org.orekit.attitudes.LofOffset
Dummy attitude law, perfectly aligned with the LOF frame.
LofOffset - Class in org.orekit.attitudes
This class provides a default attitude law.
LofOffset(RotationOrder, double, double, double) - Constructor for class org.orekit.attitudes.LofOffset
Creates new instance.
LofOffsetPointing - Class in org.orekit.attitudes
This class provides a default attitude law.
LofOffsetPointing(BodyShape, AttitudeLaw, Vector3D) - Constructor for class org.orekit.attitudes.LofOffsetPointing
Creates new instance.

M

MARS - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Mars.
MASTER_MODE - Static variable in interface org.orekit.propagation.Propagator
Indicator for master mode.
MEAN_ANOMALY - Static variable in class org.orekit.orbits.KeplerianOrbit
Identifier for mean anomaly.
MEAN_LATITUDE_ARGUMENT - Static variable in class org.orekit.orbits.EquinoctialOrbit
Identifier for mean latitude argument.
MEAN_LONGITUDE_ARGUMENT - Static variable in class org.orekit.orbits.CircularOrbit
Identifier for mean longitude argument.
MERCURY - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Mercury.
missingCoefficientsAllowed() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Check if missing coefficients are allowed in the input data.
mode - Variable in class org.orekit.propagation.numerical.NumericalPropagator
Current mode.
ModeHandler - Interface in org.orekit.propagation.numerical
Common interface for all propagator mode handlers initialization.
modeHandler - Variable in class org.orekit.propagation.numerical.NumericalPropagator
Propagator mode handler.
MODIFIED_JULIAN_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for modified julian dates: 1858-11-17T00:00:00.
MODIFIED_JULIAN_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for modified julian dates: 1858-11-17.
MOLECULAR_NITROGEN - Static variable in class org.orekit.forces.drag.DTM2000
Identifier for molecular nitrogen.
MOLECULAR_OXYGEN - Static variable in class org.orekit.forces.drag.DTM2000
Identifier for molecular oxygen.
MOON - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Moon.
MOON_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Moon equatorial radius: 1737400 m.
mu - Variable in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Central body attraction coefficient.
mu - Variable in class org.orekit.propagation.numerical.NumericalPropagator
Central body gravitational constant.

N

NadirPointing - Class in org.orekit.attitudes
This class handles nadir pointing attitude law.
NadirPointing(BodyShape) - Constructor for class org.orekit.attitudes.NadirPointing
Creates new instance.
NEPTUNE - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Neptune.
NetworkCrawler - Class in org.orekit.data
Provider for data files directly fetched from network.
NetworkCrawler(URL...) - Constructor for class org.orekit.data.NetworkCrawler
Build a data classpath crawler.
next - Variable in class org.orekit.frames.AbstractEOPHistory
Next EOP entry.
NodeDetector - Class in org.orekit.propagation.events
Finder for node crossing events.
NodeDetector(Orbit, Frame) - Constructor for class org.orekit.propagation.events.NodeDetector
Build a new instance.
NodeDetector(double, Orbit, Frame) - Constructor for class org.orekit.propagation.events.NodeDetector
Build a new instance.
normalizedC - Variable in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
fully normalized tesseral-sectorial coefficients matrix.
normalizedJ - Variable in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
fully normalized zonal coefficients array.
normalizedS - Variable in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
fully normalized tesseral-sectorial coefficients matrix.
NULL_CORRECTION - Static variable in class org.orekit.frames.NutationCorrection
Null correction (ddeps = 0, ddpsi = 0).
NULL_CORRECTION - Static variable in class org.orekit.frames.PoleCorrection
Null correction (xp = 0, yp = 0).
NumericalPropagator - Class in org.orekit.propagation.numerical
This class propagates orbits using numerical integration.
NumericalPropagator(FirstOrderIntegrator) - Constructor for class org.orekit.propagation.numerical.NumericalPropagator
Create a new instance of NumericalPropagator, based on orbit definition mu.
NumericalPropagatorWithJacobians - Class in org.orekit.propagation.numerical
This class propagates orbits using numerical integration and enables jacobians computation for orbit parameters and partial derivatives computation with respect to some force models parameters.
NumericalPropagatorWithJacobians(FirstOrderIntegrator) - Constructor for class org.orekit.propagation.numerical.NumericalPropagatorWithJacobians
Create a new instance of NumericalPropagatorWithJacobians.
NutationCorrection - Class in org.orekit.frames
Simple container class for nutation correction (IAU 1980) parameters.
NutationCorrection(double, double) - Constructor for class org.orekit.frames.NutationCorrection
Simple constructor.

O

offsetFrom(AbsoluteDate, TimeScale) - Method in class org.orekit.time.AbsoluteDate
Compute the apparent clock offset between two instant in the perspective of a specific time scale.
offsetFrom(DateTimeComponents) - Method in class org.orekit.time.DateTimeComponents
Compute the seconds offset between two instances.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.GPSScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TAIScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TCGScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TDBScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in interface org.orekit.time.TimeScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TTScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.UTCScale
Get the offset to convert locations from TAIScale to instance.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.GPSScale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.TAIScale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.TCGScale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.TDBScale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in interface org.orekit.time.TimeScale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.TTScale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.UTCScale
Get the offset to convert locations from instance to TAIScale.
omega - Variable in class org.orekit.tle.TLEPropagator
final perigee argument.
omgdot - Variable in class org.orekit.tle.TLEPropagator
common parameter for perigee argument (omega) computation.
OneAxisEllipsoid - Class in org.orekit.bodies
Modeling of a one-axis ellipsoid.
OneAxisEllipsoid(double, double, Frame) - Constructor for class org.orekit.bodies.OneAxisEllipsoid
Simple constructor.
Orbit - Class in org.orekit.orbits
This class handles orbital parameters without date.
Orbit(Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.Orbit
Default constructor.
Orbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.Orbit
Set the orbit from cartesian parameters.
OREKIT_DATA_PATH - Static variable in class org.orekit.data.DataProvidersManager
Name of the property defining the root directories or zip/jar files path for default configuration.
OrekitException - Exception in org.orekit.errors
This class is the base class for all specific exceptions thrown by the orekit classes.
OrekitException(String, Object...) - Constructor for exception org.orekit.errors.OrekitException
Simple constructor.
OrekitException(String, Throwable) - Constructor for exception org.orekit.errors.OrekitException
Simple constructor.
OrekitException(Throwable, String, Object...) - Constructor for exception org.orekit.errors.OrekitException
Simple constructor.
OrekitFixedStepHandler - Interface in org.orekit.propagation.sampling
This interface is a space-dynamics aware fixed size step handler.
OrekitStepHandler - Interface in org.orekit.propagation.sampling
This interface is a space-dynamics aware step handler.
OrekitStepInterpolator - Interface in org.orekit.propagation.sampling
This interface is a space-dynamics aware step interpolator.
OrekitStepNormalizer - Class in org.orekit.propagation.sampling
This class wraps an object implementing OrekitFixedStepHandler into a OrekitStepHandler.
OrekitStepNormalizer(double, OrekitFixedStepHandler) - Constructor for class org.orekit.propagation.sampling.OrekitStepNormalizer
Simple constructor.
org.orekit.attitudes - package org.orekit.attitudes
This package provides classes to represent simple attitudes.
org.orekit.bodies - package org.orekit.bodies
This package provides interface to represent the position and geometry of space objects such as stars, planets or asteroids.
org.orekit.data - package org.orekit.data
This package provide base classes for exploring the configured data directory tree and read external data that can be used by the library.
org.orekit.errors - package org.orekit.errors
This package provides classes to generate and handle exceptions.
org.orekit.forces - package org.orekit.forces
This package provides the interface for force models that will be used by the NumericalPropagator and the NumericalPropagatorWithJacobians, as well as some classical spacecraft models for surface forces (spherical, box and solar array ...).
org.orekit.forces.drag - package org.orekit.forces.drag
 
org.orekit.forces.gravity - package org.orekit.forces.gravity
 
org.orekit.forces.gravity.potential - package org.orekit.forces.gravity.potential
This package provides classes to read gravity field files and supports several different formats.
org.orekit.forces.maneuvers - package org.orekit.forces.maneuvers
This package provides models of simple maneuvers.
org.orekit.forces.radiation - package org.orekit.forces.radiation
 
org.orekit.frames - package org.orekit.frames
This package provides classes to handle frames and transforms between them.
org.orekit.orbits - package org.orekit.orbits
This package provides classes to represent orbits.
org.orekit.propagation - package org.orekit.propagation
This package provides tools to propagate orbital states with different methods.
org.orekit.propagation.analytical - package org.orekit.propagation.analytical
 
org.orekit.propagation.events - package org.orekit.propagation.events
This package provides interfaces and classes dealing with events occurring during propagation.
org.orekit.propagation.numerical - package org.orekit.propagation.numerical
 
org.orekit.propagation.sampling - package org.orekit.propagation.sampling
This package provides interfaces and classes dealing with step handling during propagation.
org.orekit.time - package org.orekit.time
This independent package provides classes to handle epochs, time scales, and to compare instants together.
org.orekit.tle - package org.orekit.tle
This package provides classes to read and extrapolate tle's.
org.orekit.utils - package org.orekit.utils
This package provides useful objects.

P

Parameterizable - Interface in org.orekit.forces
This interface enables to process partial derivatives with respect to force model parameters.
parseDate(String) - Static method in class org.orekit.time.DateComponents
Parse a string in ISO-8601 format to build a date.
parseDateTime(String) - Static method in class org.orekit.time.DateTimeComponents
Parse a string in ISO-8601 format to build a date/time.
parseTime(String) - Static method in class org.orekit.time.TimeComponents
Parse a string in ISO-8601 format to build a time.
PAST_INFINITY - Static variable in class org.orekit.time.AbsoluteDate
Dummy date at infinity in the past direction.
perige - Variable in class org.orekit.tle.TLEPropagator
perigee, expressed in KM and ALTITUDE.
PLUTO - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Pluto.
pointAt(double) - Method in class org.orekit.utils.Line
Get one point from the line.
PoissonSeries - Class in org.orekit.data
Class representing a Poisson series for nutation or ephemeris computations.
PoissonSeries(InputStream, double, String) - Constructor for class org.orekit.data.PoissonSeries
Build a Poisson series from an IERS table file.
PoleCorrection - Class in org.orekit.frames
Simple container class for pole correction parameters.
PoleCorrection(double, double) - Constructor for class org.orekit.frames.PoleCorrection
Simple constructor.
PotentialCoefficientsProvider - Interface in org.orekit.forces.gravity.potential
Interface used to provide gravity field coefficients.
PotentialCoefficientsReader - Class in org.orekit.forces.gravity.potential
This abstract class represents a Gravitational Potential Coefficients file reader.
PotentialCoefficientsReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Simple constructor.
PotentialReaderFactory - Class in org.orekit.forces.gravity.potential
Deprecated. as of 4.2, replaced by GravityFieldFactory
PotentialReaderFactory() - Constructor for class org.orekit.forces.gravity.potential.PotentialReaderFactory
Deprecated. Simple constructor.
PotentialReaderFactory(String, String, String, String) - Constructor for class org.orekit.forces.gravity.potential.PotentialReaderFactory
Deprecated. Simple constructor.
prepareInterpolation(AbsoluteDate) - Method in class org.orekit.frames.AbstractEOPHistory
Prepare interpolation between two entries.
previous - Variable in class org.orekit.frames.AbstractEOPHistory
Previous EOP entry.
propagate(AbsoluteDate) - Method in class org.orekit.propagation.AbstractPropagator
Propagate towards a target date.
propagate(AbsoluteDate) - Method in interface org.orekit.propagation.BasicPropagator
Propagate towards a target date.
propagate(AbsoluteDate) - Method in class org.orekit.propagation.Ephemeris
Propagate towards a target date.
propagate(AbsoluteDate) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Propagate towards a target date.
propagate(AbsoluteDate, double[][], double[][]) - Method in class org.orekit.propagation.numerical.NumericalPropagatorWithJacobians
Propagate towards a target date and compute partial derivatives.
PropagationException - Exception in org.orekit.errors
This class is the base class for all specific exceptions thrown by during the propagation computation.
PropagationException(String, Object...) - Constructor for exception org.orekit.errors.PropagationException
Simple constructor.
PropagationException(String, Throwable) - Constructor for exception org.orekit.errors.PropagationException
Simple constructor.
Propagator - Interface in org.orekit.propagation
This interface provides a way to propagate an orbit at any time.
PVCoordinates - Class in org.orekit.utils
Simple container for Position/Velocity pairs.
PVCoordinates() - Constructor for class org.orekit.utils.PVCoordinates
Simple constructor.
PVCoordinates(Vector3D, Vector3D) - Constructor for class org.orekit.utils.PVCoordinates
Builds a PVCoordinates pair.
PVCoordinates(double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates
Multiplicative constructor
PVCoordinates(PVCoordinates, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates
Subtractive constructor
PVCoordinates(double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates
Linear constructor
PVCoordinates(double, PVCoordinates, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates
Linear constructor
PVCoordinates(double, PVCoordinates, double, PVCoordinates, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates
Linear constructor
PVCoordinatesProvider - Interface in org.orekit.utils
Interface for PV coordinates providers.

R

radiationPressureAcceleration(SpacecraftState, Vector3D) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(SpacecraftState, Vector3D) - Method in interface org.orekit.forces.radiation.RadiationSensitive
Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(SpacecraftState, Vector3D) - Method in class org.orekit.forces.SphericalSpacecraft
Compute the acceleration due to radiation pressure.
RadiationSensitive - Interface in org.orekit.forces.radiation
Interface for spacecraft that are sensitive to radiation pressure forces.
readCompleted - Variable in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Indicator for completed read.
REFLECTION_COEFFICIENT - Static variable in class org.orekit.forces.radiation.SolarRadiationPressure
Parameter name for specular reflection coefficient enabling jacobian processing.
removeForceModels() - Method in class org.orekit.propagation.numerical.NumericalPropagator
Remove all perturbing force models from the global perturbation model.
removeForceModels() - Method in class org.orekit.propagation.numerical.NumericalPropagatorWithJacobians
Remove all perturbing force models from the global perturbation model.
removeProvider(Class<? extends DataProvider>) - Method in class org.orekit.data.DataProvidersManager
Remove one provider.
requiresDenseOutput() - Method in class org.orekit.propagation.sampling.AdaptedStepHandler
requiresDenseOutput() - Method in interface org.orekit.propagation.sampling.OrekitStepHandler
Determines whether this handler needs dense output.
requiresDenseOutput() - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer
Determines whether this handler needs dense output.
reset(SpacecraftState) - Method in class org.orekit.propagation.events.CombinedEventsDetectorsManager
Let the events detectors reset the state if they want.
reset() - Method in class org.orekit.propagation.sampling.AdaptedStepHandler
reset() - Method in interface org.orekit.propagation.sampling.OrekitStepHandler
Reset the step handler.
reset() - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer
Reset the step handler.
RESET_DERIVATIVES - Static variable in interface org.orekit.propagation.events.EventDetector
Reset derivatives indicator.
RESET_STATE - Static variable in interface org.orekit.propagation.events.EventDetector
Reset state indicator.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.KeplerianPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in interface org.orekit.propagation.Propagator
Reset the propagator initial state.
resetState(SpacecraftState) - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Reset the state prior to continue propagation.
resetState(SpacecraftState) - Method in class org.orekit.propagation.events.AbstractDetector
Reset the state prior to continue propagation.
resetState(double, double[]) - Method in class org.orekit.propagation.events.AdaptedEventDetector
resetState(SpacecraftState) - Method in interface org.orekit.propagation.events.EventDetector
Reset the state prior to continue propagation.
revert(Line) - Static method in class org.orekit.utils.Line
Revert the line direction.

S

s4 - Variable in class org.orekit.tle.TLEPropagator
s* new value for the contant s.
SATURN - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Saturn.
SDP4 - Static variable in class org.orekit.tle.TLE
Identifier for SDP4 type of ephemeris.
SDP8 - Static variable in class org.orekit.tle.TLE
Identifier for SDP8 type of ephemeris.
selectBracketingEntries(AbsoluteDate) - Method in class org.orekit.frames.AbstractEOPHistory
Select the entries bracketing a specified date.
selectExtrapolator(TLE) - Static method in class org.orekit.tle.TLEPropagator
Selects the extrapolator to use with the selected TLE.
selectParameters(String[]) - Method in class org.orekit.propagation.numerical.NumericalPropagatorWithJacobians
Select the parameters to consider for jacobian processing.
SeriesTerm - Class in org.orekit.data
Base class for nutation series terms.
SeriesTerm(double, double) - Constructor for class org.orekit.data.SeriesTerm
Simple constructor for the base class.
setAbsorptionCoefficient(double) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Set the absorption coefficient.
setAbsorptionCoefficient(double) - Method in interface org.orekit.forces.radiation.RadiationSensitive
Set the absorption coefficient.
setAbsorptionCoefficient(double) - Method in class org.orekit.forces.SphericalSpacecraft
Set the absorption coefficient.
setAngularThreshold(double) - Method in class org.orekit.bodies.OneAxisEllipsoid
Set the angular convergence threshold.
setAttitudeLaw(AttitudeLaw) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Set the attitude law.
setCloseApproachThreshold(double) - Method in class org.orekit.bodies.OneAxisEllipsoid
Set the close approach threshold.
setDragCoefficient(double) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Set the drag coefficient.
setDragCoefficient(double) - Method in interface org.orekit.forces.drag.DragSensitive
Set the drag coefficient.
setDragCoefficient(double) - Method in class org.orekit.forces.SphericalSpacecraft
Set the drag coefficient.
setEphemerisMode() - Method in class org.orekit.propagation.AbstractPropagator
Set the propagator to ephemeris generation mode.
setEphemerisMode() - Method in class org.orekit.propagation.numerical.NumericalPropagator
Set the propagator to ephemeris generation mode.
setEphemerisMode() - Method in interface org.orekit.propagation.Propagator
Set the propagator to ephemeris generation mode.
setInitialState(SpacecraftState) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Set the initial state.
setIntegrator(FirstOrderIntegrator) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Set the integrator.
setInterpolatedDate(AbsoluteDate) - Method in class org.orekit.propagation.sampling.AdaptedStepHandler
Set the interpolated date.
setInterpolatedDate(AbsoluteDate) - Method in class org.orekit.propagation.sampling.BasicStepInterpolator
Set the interpolated date.
setInterpolatedDate(AbsoluteDate) - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
Set the interpolated date.
setMasterMode(double, OrekitFixedStepHandler) - Method in class org.orekit.propagation.AbstractPropagator
Set the propagator to master mode with fixed steps.
setMasterMode(OrekitStepHandler) - Method in class org.orekit.propagation.AbstractPropagator
Set the propagator to master mode with variable steps.
setMasterMode(double, OrekitFixedStepHandler) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Set the propagator to master mode with fixed steps.
setMasterMode(OrekitStepHandler) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Set the propagator to master mode with variable steps.
setMasterMode(double, OrekitFixedStepHandler) - Method in interface org.orekit.propagation.Propagator
Set the propagator to master mode with fixed steps.
setMasterMode(OrekitStepHandler) - Method in interface org.orekit.propagation.Propagator
Set the propagator to master mode with variable steps.
setMu(double) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Set the central attraction coefficient μ.
setParameter(String, double) - Method in class org.orekit.forces.drag.DragForce
Set the value for a given parameter.
setParameter(String, double) - Method in interface org.orekit.forces.Parameterizable
Set the value for a given parameter.
setParameter(String, double) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Set the value for a given parameter.
setReflectionCoefficient(double) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Set the specular reflection coefficient.
setReflectionCoefficient(double) - Method in interface org.orekit.forces.radiation.RadiationSensitive
Set the specular reflection coefficient.
setReflectionCoefficient(double) - Method in class org.orekit.forces.SphericalSpacecraft
Set the specular reflection coefficient.
setSlaveMode() - Method in class org.orekit.propagation.AbstractPropagator
Set the propagator to slave mode.
setSlaveMode() - Method in class org.orekit.propagation.numerical.NumericalPropagator
Set the propagator to slave mode.
setSlaveMode() - Method in interface org.orekit.propagation.Propagator
Set the propagator to slave mode.
setTimeout(int) - Method in class org.orekit.data.NetworkCrawler
Set the timeout for connection.
setTransform(Transform) - Method in class org.orekit.frames.Frame
Update the transform from the parent frame to the instance.
setUpEventDetector(EventDetector) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Wrap an Orekit event detector and register it to the integrator.
SGP - Static variable in class org.orekit.tle.TLE
Identifier for SGP type of ephemeris.
SGP4 - Static variable in class org.orekit.tle.TLE
Identifier for SGP4 type of ephemeris.
SGP8 - Static variable in class org.orekit.tle.TLE
Identifier for SGP8 type of ephemeris.
shift() - Method in class org.orekit.propagation.sampling.BasicStepInterpolator
Shift one step forward.
shiftedBy(double) - Method in class org.orekit.attitudes.Attitude
Get a time-shifted attitude.
shiftedBy(double) - Method in class org.orekit.orbits.CartesianOrbit
Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.CircularOrbit
Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.EquinoctialOrbit
Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.KeplerianOrbit
Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.Orbit
Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.propagation.SpacecraftState
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.time.AbsoluteDate
Get a time-shifted date.
shiftedBy(double) - Method in class org.orekit.utils.PVCoordinates
Get a time-shifted state.
SHM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory
Default regular expression for SHM files.
SHMFormatReader - Class in org.orekit.forces.gravity.potential
Reader for the SHM gravity field format.
SHMFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.SHMFormatReader
Simple constructor.
SimpleExponentialAtmosphere - Class in org.orekit.forces.drag
Simple exponential atmospheric model.
SimpleExponentialAtmosphere(BodyShape, Frame, double, double, double) - Constructor for class org.orekit.forces.drag.SimpleExponentialAtmosphere
Create an exponential atmosphere.
sini0 - Variable in class org.orekit.tle.TLEPropagator
sinus original inclination.
SLAVE_MODE - Static variable in interface org.orekit.propagation.Propagator
Indicator for slave mode.
SOLAR_SYSTEM_BARYCENTER - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for solar system barycenter.
SolarRadiationPressure - Class in org.orekit.forces.radiation
Solar radiation pressure force model.
SolarRadiationPressure(PVCoordinatesProvider, double, RadiationSensitive) - Constructor for class org.orekit.forces.radiation.SolarRadiationPressure
Simple constructor with default reference values.
SolarRadiationPressure(double, double, PVCoordinatesProvider, double, RadiationSensitive) - Constructor for class org.orekit.forces.radiation.SolarRadiationPressure
Complete constructor.
SolarSystemBody - Class in org.orekit.bodies
Deprecated. since 4.2 replaced by CelestialBodyFactory
SpacecraftFrame - Class in org.orekit.frames
Spacecraft frame.
SpacecraftFrame(Propagator, String) - Constructor for class org.orekit.frames.SpacecraftFrame
Simple constructor.
SpacecraftState - Class in org.orekit.propagation
This class is the representation of a complete state holding orbit, attitude and mass information at a given date.
SpacecraftState(Orbit) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from orbit only.
SpacecraftState(Orbit, Attitude) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from orbit and attitude law.
SpacecraftState(Orbit, double) - Constructor for class org.orekit.propagation.SpacecraftState
Create a new instance from orbit and mass.
SpacecraftState(Orbit, Attitude, double) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from orbit, attitude law and mass.
SPEED_OF_LIGHT - Static variable in interface org.orekit.utils.Constants
Speed of light: 299792458.0 m/s.
SphericalSpacecraft - Class in org.orekit.forces
This class represents the features of a simplified spacecraft.
SphericalSpacecraft(double, double, double, double) - Constructor for class org.orekit.forces.SphericalSpacecraft
Simple constructor.
SpinStabilized - Class in org.orekit.attitudes
This class handles a spin stabilized attitude law.
SpinStabilized(AttitudeLaw, AbsoluteDate, Vector3D, double) - Constructor for class org.orekit.attitudes.SpinStabilized
Creates a new instance.
startDate - Variable in class org.orekit.propagation.numerical.NumericalPropagator
Start date.
stateVector - Variable in class org.orekit.propagation.numerical.NumericalPropagator
State vector.
stepAccepted(SpacecraftState) - Method in class org.orekit.propagation.events.CombinedEventsDetectorsManager
Inform the events detectors that the step has been accepted by the propagator.
stillAcceptsData() - Method in class org.orekit.bodies.JPLEphemeridesLoader
Check if the loader still accepts new data.
stillAcceptsData() - Method in interface org.orekit.data.DataLoader
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.tle.TLESeries
Check if the loader still accepts new data.
stop() - Method in class org.orekit.propagation.events.CombinedEventsDetectorsManager
Check if the propagation should be stopped at the end of the current step.
STOP - Static variable in interface org.orekit.propagation.events.EventDetector
Stop indicator.
storeDate(AbsoluteDate) - Method in class org.orekit.propagation.sampling.BasicStepInterpolator
Store the current step date.
SUN - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Sun.
SUN_RADIUS - Static variable in interface org.orekit.utils.Constants
Sun radius: 695500000 m.
sxpInitialize() - Method in class org.orekit.tle.TLEPropagator
Initialization proper to each propagator (SGP or SDP).
sxpPropagate(double) - Method in class org.orekit.tle.TLEPropagator
Propagation proper to each propagator (SGP or SDP).

T

t2cof - Variable in class org.orekit.tle.TLEPropagator
3/2 * C1.
TAIScale - Class in org.orekit.time
International Atomic Time.
TargetPointing - Class in org.orekit.attitudes
This class handles target pointing attitude law.
TargetPointing(Frame, Vector3D) - Constructor for class org.orekit.attitudes.TargetPointing
Creates a new instance from body frame and target expressed in cartesian coordinates.
TargetPointing(GeodeticPoint, BodyShape) - Constructor for class org.orekit.attitudes.TargetPointing
Creates a new instance from body shape and target expressed in geodetic coordinates.
TCGScale - Class in org.orekit.time
Geocentric Coordinate Time.
TDBScale - Class in org.orekit.time
Barycentric Dynamic Time.
theta2 - Variable in class org.orekit.tle.TLEPropagator
cos io squared.
ThirdBodyAttraction - Class in org.orekit.forces.gravity
Third body attraction force model.
ThirdBodyAttraction(CelestialBody) - Constructor for class org.orekit.forces.gravity.ThirdBodyAttraction
Simple constructor.
TidalCorrection - Class in org.orekit.frames
Compute tidal correction to the pole motion.
TidalCorrection() - Constructor for class org.orekit.frames.TidalCorrection
Simple constructor.
TimeComponents - Class in org.orekit.time
Class representing a time within the day broken up as hour, minute and second components.
TimeComponents(int, int, double) - Constructor for class org.orekit.time.TimeComponents
Build a time from its clock elements.
TimeComponents(double) - Constructor for class org.orekit.time.TimeComponents
Build a time from the second number within the day.
TimeDerivativesEquations - Class in org.orekit.propagation.numerical
This class sums up the contribution of several forces into orbit and mass derivatives.
TimeDerivativesEquations(EquinoctialOrbit) - Constructor for class org.orekit.propagation.numerical.TimeDerivativesEquations
Create a new instance.
TimeDerivativesEquationsWithJacobians - Class in org.orekit.propagation.numerical
This class sums up the contribution of several forces into orbit and mass derivatives and partial derivatives.
TimeDerivativesEquationsWithJacobians(EquinoctialOrbit) - Constructor for class org.orekit.propagation.numerical.TimeDerivativesEquationsWithJacobians
Create a new instance.
TimeScale - Interface in org.orekit.time
Interface for time scales.
TimeScalesFactory - Class in org.orekit.time
Factory for predefined time scales.
timeScalesOffset(TimeScale, TimeScale) - Method in class org.orekit.time.AbsoluteDate
Compute the offset between two time scales at the current instant.
TimeStamped - Interface in org.orekit.time
This interface represents objects that have a AbsoluteDate date attached to them.
TLE - Class in org.orekit.tle
This class is a container for a single set of TLE data.
TLE(String, String) - Constructor for class org.orekit.tle.TLE
Simple constructor from unparsed two lines.
TLE(int, char, int, int, String, int, int, AbsoluteDate, double, double, double, double, double, double, double, double, int, double) - Constructor for class org.orekit.tle.TLE
Simple constructor from already parsed elements.
tle - Variable in class org.orekit.tle.TLEPropagator
Initial state.
TLEPropagator - Class in org.orekit.tle
This class provides elements to propagate TLE's.
TLEPropagator(TLE) - Constructor for class org.orekit.tle.TLEPropagator
Protected constructor for derived classes.
TLESeries - Class in org.orekit.tle
This class reads and handles series of TLEs for one space object.
TLESeries(InputStream) - Constructor for class org.orekit.tle.TLESeries
Deprecated. since 4.2 replaced by "new TLESeries.TLESeries(String, boolean).TLESeries.loadTLEData()"
TLESeries(String, boolean) - Constructor for class org.orekit.tle.TLESeries
Simple constructor with a TLE file.
toDate(TimeScale) - Method in class org.orekit.time.AbsoluteDate
Convert the instance to a Java Date.
TopocentricFrame - Class in org.orekit.frames
Topocentric frame.
TopocentricFrame(BodyShape, GeodeticPoint, String) - Constructor for class org.orekit.frames.TopocentricFrame
Simple constructor.
toString() - Method in class org.orekit.frames.Frame
New definition of the java.util toString() method.
toString() - Method in class org.orekit.orbits.CartesianOrbit
Returns a string representation of this Orbit object.
toString() - Method in class org.orekit.orbits.CircularOrbit
Returns a string representation of this Orbit object.
toString() - Method in class org.orekit.orbits.EquinoctialOrbit
Returns a string representation of this equinoctial parameters object.
toString() - Method in class org.orekit.orbits.KeplerianOrbit
Returns a string representation of this keplerian parameters object.
toString() - Method in class org.orekit.time.AbsoluteDate
Get a String representation of the instant location in UTC time scale.
toString(TimeScale) - Method in class org.orekit.time.AbsoluteDate
Get a String representation of the instant location.
toString() - Method in class org.orekit.time.DateComponents
Get a string representation (ISO-8601) of the date.
toString() - Method in class org.orekit.time.DateTimeComponents
Return a string representation of this pair.
toString() - Method in class org.orekit.time.GPSScale
toString() - Method in class org.orekit.time.TAIScale
toString() - Method in class org.orekit.time.TCGScale
toString() - Method in class org.orekit.time.TDBScale
toString() - Method in class org.orekit.time.TimeComponents
Get a string representation of the time.
toString() - Method in class org.orekit.time.TTScale
toString() - Method in class org.orekit.time.UTCScale
toString() - Method in class org.orekit.tle.TLE
Get a string representation of this TLE set.
toString() - Method in class org.orekit.utils.PVCoordinates
Return a string representation of this position/velocity pair.
toTransform() - Method in class org.orekit.propagation.SpacecraftState
Compute the transform from orbite/attitude reference frame to spacecraft frame.
transform(Vector3D, Frame, AbsoluteDate) - Method in interface org.orekit.bodies.BodyShape
Transform a cartesian point to a surface-relative point.
transform(GeodeticPoint) - Method in interface org.orekit.bodies.BodyShape
Transform a surface-relative point to a cartesian point.
transform(GeodeticPoint) - Method in class org.orekit.bodies.OneAxisEllipsoid
Transform a surface-relative point to a cartesian point.
transform(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.bodies.OneAxisEllipsoid
Transform a cartesian point to a surface-relative point.
Transform - Class in org.orekit.frames
Transformation class in three dimensional space.
Transform(Vector3D) - Constructor for class org.orekit.frames.Transform
Build a translation transform.
Transform(Rotation) - Constructor for class org.orekit.frames.Transform
Build a rotation transform.
Transform(Vector3D, Vector3D) - Constructor for class org.orekit.frames.Transform
Build a translation transform, with its first time derivative.
Transform(Rotation, Vector3D) - Constructor for class org.orekit.frames.Transform
Build a rotation transform.
Transform(Transform, Transform) - Constructor for class org.orekit.frames.Transform
Build a transform by combining two existing ones.
transformLine(Line) - Method in class org.orekit.frames.Transform
Transform a line.
transformPosition(Vector3D) - Method in class org.orekit.frames.Transform
Transform a position vector (including translation effects).
transformPVCoordinates(PVCoordinates) - Method in class org.orekit.frames.Transform
Transform PVCoordinates including kinematic effects.
transformVector(Vector3D) - Method in class org.orekit.frames.Transform
Transform a vector (ignoring translation effects).
TRUE_ANOMALY - Static variable in class org.orekit.orbits.KeplerianOrbit
Identifier for true anomaly.
TRUE_LATITUDE_ARGUMENT - Static variable in class org.orekit.orbits.EquinoctialOrbit
Identifier for true latitude argument.
TRUE_LONGITUDE_ARGUMENT - Static variable in class org.orekit.orbits.CircularOrbit
Identifier for true longitude argument.
tsi - Variable in class org.orekit.tle.TLEPropagator
tsi from SPTRCK #3.
TTScale - Class in org.orekit.time
Terrestrial Time as defined by IAU(1991) recommendation IV.

U

updateFrame(AbsoluteDate) - Method in class org.orekit.frames.Frame
Update the frame to the given date.
updateFrame(AbsoluteDate) - Method in class org.orekit.frames.LocalOrbitalFrame
Update the frame to the given date.
updateFrame(AbsoluteDate) - Method in class org.orekit.frames.SpacecraftFrame
Update the frame to the given date.
updateTransform(Frame, Frame, Transform, AbsoluteDate) - Method in class org.orekit.frames.Frame
Update the transform from parent frame implicitly according to two other frames.
URANUS - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Uranus.
UTCScale - Class in org.orekit.time
Coordinated Universal Time.
UTCTAILoader - Interface in org.orekit.time
Interface for loading UTC-TAI offsets data files.

V

value(double, BodiesElements) - Method in class org.orekit.data.PoissonSeries
Compute the value of the development for the current date.
value(BodiesElements) - Method in class org.orekit.data.SeriesTerm
Compute the value of the term for the current date.
valueOf(String) - Static method in enum org.orekit.bodies.JPLEphemeridesLoader.EphemerisType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.frames.LocalOrbitalFrame.LOFType
Returns the enum constant of this type with the specified name.
values() - Static method in enum org.orekit.bodies.JPLEphemeridesLoader.EphemerisType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.frames.LocalOrbitalFrame.LOFType
Returns an array containing the constants of this enum type, in the order they are declared.
VENUS - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Venus.

W

WGS84_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants
Earth angular velocity from WGS84 model: 7.292115e-5 rad/s.
WGS84_EARTH_C20 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized second zonal coefficient from WGS84 model: .
WGS84_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth equatorial radius from WGS84 model: 6378137.0 m.
WGS84_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants
Earth flattening from WGS84 model: 1.0 / 298.257223563.
WGS84_EARTH_MU - Static variable in interface org.orekit.utils.Constants
Earth gravitational constant from WGS84 model: 3.986004418 m3/s2.
withReferenceFrame(Frame) - Method in class org.orekit.attitudes.Attitude
Get a similar attitude with a specific reference frame.

X

xl - Variable in class org.orekit.tle.TLEPropagator
L from SPTRCK #3.
xmdot - Variable in class org.orekit.tle.TLEPropagator
common parameter for mean anomaly (M) computation.
xn0dp - Variable in class org.orekit.tle.TLEPropagator
original recovered mean motion.
xnodcf - Variable in class org.orekit.tle.TLEPropagator
common parameter for raan (OMEGA) computation.
xnode - Variable in class org.orekit.tle.TLEPropagator
final RAAN.
xnodot - Variable in class org.orekit.tle.TLEPropagator
common parameter for raan (OMEGA) computation.

Y

YawCompensation - Class in org.orekit.attitudes
This class handles yaw compensation attitude law.
YawCompensation(GroundPointing) - Constructor for class org.orekit.attitudes.YawCompensation
Creates a new instance.
YawSteering - Class in org.orekit.attitudes
This class handles yaw steering law.
YawSteering(GroundPointing, PVCoordinatesProvider, Vector3D) - Constructor for class org.orekit.attitudes.YawSteering
Creates a new instance.

Z

ZERO - Static variable in class org.orekit.utils.PVCoordinates
Fixed position/velocity at origin (both p and v are zero vectors).
ZIP_ARCHIVE_PATTERN - Static variable in interface org.orekit.data.DataProvider
Pattern for name of zip/jar archives.
ZipJarCrawler - Class in org.orekit.data
Helper class for loading data files from a zip/jar archive.
ZipJarCrawler(File) - Constructor for class org.orekit.data.ZipJarCrawler
Build a zip crawler for an archive file on filesystem.
ZipJarCrawler(String) - Constructor for class org.orekit.data.ZipJarCrawler
Build a zip crawler for an archive file in classpath.
ZipJarCrawler(URL) - Constructor for class org.orekit.data.ZipJarCrawler
Build a zip crawler for an archive file on network.
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