Uses of Interface
org.orekit.bodies.CelestialBody

Packages that use CelestialBody

Package	Description
org.orekit.bodies	This package provides interface to represent the position and geometry of space objects such as stars, planets or asteroids.
org.orekit.files.ccsds.definitions	This package contains definitions for CCSDS objects (frames, time systems...).
org.orekit.files.general	This package provides interfaces for orbit file representations and corresponding parsers.
org.orekit.forces.gravity	This package provides all gravity-related forces.
org.orekit.frames	This package provides classes to handle frames and transforms between them.
org.orekit.propagation.semianalytical.dsst.forces	This package provides force models for Draper Semi-analytical Satellite Theory (DSST).

Uses of CelestialBody in org.orekit.bodies

Methods in org.orekit.bodies that return CelestialBody

Modifier and Type	Method	Description
CelestialBody	CelestialBodies.getBody(String name)	Get a celestial body.
static CelestialBody	CelestialBodyFactory.getBody(String name)	Get a celestial body.
CelestialBody	LazyLoadedCelestialBodies.getBody(String name)	Get a celestial body.
CelestialBody	CelestialBodies.getEarth()	Get the Earth singleton body.
static CelestialBody	CelestialBodyFactory.getEarth()	Get the Earth singleton body.
CelestialBody	LazyLoadedCelestialBodies.getEarth()
CelestialBody	CelestialBodies.getEarthMoonBarycenter()	Get the Earth-Moon barycenter singleton bodies pair.
static CelestialBody	CelestialBodyFactory.getEarthMoonBarycenter()	Get the Earth-Moon barycenter singleton bodies pair.
CelestialBody	LazyLoadedCelestialBodies.getEarthMoonBarycenter()
CelestialBody	CelestialBodies.getJupiter()	Get the Jupiter singleton body.
static CelestialBody	CelestialBodyFactory.getJupiter()	Get the Jupiter singleton body.
CelestialBody	LazyLoadedCelestialBodies.getJupiter()
CelestialBody	CelestialBodies.getMars()	Get the Mars singleton body.
static CelestialBody	CelestialBodyFactory.getMars()	Get the Mars singleton body.
CelestialBody	LazyLoadedCelestialBodies.getMars()
CelestialBody	CelestialBodies.getMercury()	Get the Mercury singleton body.
static CelestialBody	CelestialBodyFactory.getMercury()	Get the Mercury singleton body.
CelestialBody	LazyLoadedCelestialBodies.getMercury()
CelestialBody	CelestialBodies.getMoon()	Get the Moon singleton body.
static CelestialBody	CelestialBodyFactory.getMoon()	Get the Moon singleton body.
CelestialBody	LazyLoadedCelestialBodies.getMoon()
CelestialBody	CelestialBodies.getNeptune()	Get the Neptune singleton body.
static CelestialBody	CelestialBodyFactory.getNeptune()	Get the Neptune singleton body.
CelestialBody	LazyLoadedCelestialBodies.getNeptune()
CelestialBody	CelestialBodies.getPluto()	Get the Pluto singleton body.
static CelestialBody	CelestialBodyFactory.getPluto()	Get the Pluto singleton body.
CelestialBody	LazyLoadedCelestialBodies.getPluto()
CelestialBody	CR3BPSystem.getPrimary()	Get the primary CelestialBody.
CelestialBody	CelestialBodies.getSaturn()	Get the Saturn singleton body.
static CelestialBody	CelestialBodyFactory.getSaturn()	Get the Saturn singleton body.
CelestialBody	LazyLoadedCelestialBodies.getSaturn()
CelestialBody	CR3BPSystem.getSecondary()	Get the secondary CelestialBody.
CelestialBody	CelestialBodies.getSolarSystemBarycenter()	Get the solar system barycenter aggregated body.
static CelestialBody	CelestialBodyFactory.getSolarSystemBarycenter()	Get the solar system barycenter aggregated body.
CelestialBody	LazyLoadedCelestialBodies.getSolarSystemBarycenter()
CelestialBody	CelestialBodies.getSun()	Get the Sun singleton body.
static CelestialBody	CelestialBodyFactory.getSun()	Get the Sun singleton body.
CelestialBody	LazyLoadedCelestialBodies.getSun()
CelestialBody	CelestialBodies.getUranus()	Get the Uranus singleton body.
static CelestialBody	CelestialBodyFactory.getUranus()	Get the Uranus singleton body.
CelestialBody	LazyLoadedCelestialBodies.getUranus()
CelestialBody	CelestialBodies.getVenus()	Get the Venus singleton body.
static CelestialBody	CelestialBodyFactory.getVenus()	Get the Venus singleton body.
CelestialBody	LazyLoadedCelestialBodies.getVenus()
CelestialBody	CelestialBodyLoader.loadCelestialBody(String name)	Load celestial body.
CelestialBody	JPLEphemeridesLoader.loadCelestialBody(String name)	Load celestial body.

Methods in org.orekit.bodies with parameters of type CelestialBody

Modifier and Type	Method	Description
static CR3BPSystem	CR3BPFactory.getSystem(CelestialBody primaryBody, CelestialBody secondaryBody, double a)	Get the corresponding CR3BP System.

Constructors in org.orekit.bodies with parameters of type CelestialBody

Constructor	Description
CR3BPSystem(CelestialBody primaryBody, CelestialBody secondaryBody, double a)	Simple constructor.
CR3BPSystem(CelestialBody primaryBody, CelestialBody secondaryBody, double a, double mu)	Simple constructor.

Uses of CelestialBody in org.orekit.files.ccsds.definitions

Methods in org.orekit.files.ccsds.definitions that return CelestialBody

Modifier and Type	Method	Description
CelestialBody	BodyFacade.getBody()	Get the celestial body.
CelestialBody	CenterName.getCelestialBody()	Get the celestial body corresponding to the CCSDS constant.
CelestialBody	CenterName.getCelestialBody(CelestialBodies celestialBodies)	Get the celestial body corresponding to the CCSDS constant.

Constructors in org.orekit.files.ccsds.definitions with parameters of type CelestialBody

Constructor	Description
BodyFacade(String name, CelestialBody body)	Simple constructor.
ModifiedFrame(Frame frame, CelestialBodyFrame refFrame, CelestialBody body, String centerName)	Create a CCSDS reference frame by changing the origin of an existing frame.

Uses of CelestialBody in org.orekit.files.general

Methods in org.orekit.files.general with parameters of type CelestialBody

Modifier and Type	Method	Description
OrekitEphemerisFile.OrekitEphemerisSegment	OrekitEphemerisFile.OrekitSatelliteEphemeris.addNewSegment(List<SpacecraftState> states, CelestialBody body, int interpolationSampleSize)	Injects pre-computed satellite states into this ephemeris file object, returning the generated OrekitEphemerisFile.OrekitEphemerisSegment that has been stored internally.
OrekitEphemerisFile.OrekitEphemerisSegment	OrekitEphemerisFile.OrekitSatelliteEphemeris.addNewSegment(List<SpacecraftState> states, CelestialBody body, int interpolationSampleSize, TimeScale timeScale)	Injects pre-computed satellite states into this ephemeris file object, returning the generated OrekitEphemerisFile.OrekitEphemerisSegment that has been stored internally.

Uses of CelestialBody in org.orekit.forces.gravity

Methods in org.orekit.forces.gravity that return CelestialBody

Modifier and Type	Method	Description
protected CelestialBody	AbstractBodyAttraction.getBody()	Deprecated. in next major release this shall be removed as the class will not have to use a CelestialBody
CelestialBody	DeSitterRelativity.getEarth()	Get the Earth model used to compute De Sitter effect.
CelestialBody	DeSitterRelativity.getSun()	Get the sun model used to compute De Sitter effect.

Constructors in org.orekit.forces.gravity with parameters of type CelestialBody

Constructor	Description
AbstractBodyAttraction(CelestialBody body)	Simple constructor.
DeSitterRelativity(CelestialBody earth, CelestialBody sun)	Simple constructor.
SingleBodyAbsoluteAttraction(CelestialBody body)	Simple constructor.
SingleBodyRelativeAttraction(CelestialBody body)	Simple constructor.
SolidTides(Frame centralBodyFrame, double ae, double mu, TideSystem centralTideSystem, boolean poleTide, double step, int nbPoints, IERSConventions conventions, UT1Scale ut1, CelestialBody... bodies)	Simple constructor.
SolidTides(Frame centralBodyFrame, double ae, double mu, TideSystem centralTideSystem, IERSConventions conventions, UT1Scale ut1, CelestialBody... bodies)	Simple constructor.
ThirdBodyAttraction(CelestialBody body)	Simple constructor.
ThirdBodyAttractionEpoch(CelestialBody body)	Simple constructor.

Uses of CelestialBody in org.orekit.frames

Constructors in org.orekit.frames with parameters of type CelestialBody

Constructor	Description
CR3BPRotatingFrame(double mu, CelestialBody primaryBody, CelestialBody secondaryBody)	Simple constructor.
L1Frame(CelestialBody primaryBody, CelestialBody secondaryBody)	Simple constructor.
L1TransformProvider(CelestialBody primaryBody, CelestialBody secondaryBody)	Simple constructor.
L2Frame(CelestialBody primaryBody, CelestialBody secondaryBody)	Simple constructor.
TwoBodiesBaryFrame(CelestialBody primaryBody, CelestialBody secondaryBody)	Simple constructor.

Uses of CelestialBody in org.orekit.propagation.semianalytical.dsst.forces

Methods in org.orekit.propagation.semianalytical.dsst.forces that return CelestialBody

Modifier and Type	Method	Description
CelestialBody	DSSTThirdBody.getBody()	Get third body.

Constructors in org.orekit.propagation.semianalytical.dsst.forces with parameters of type CelestialBody

Constructor	Description
DSSTThirdBody(CelestialBody body, double mu)	Complete constructor.
DSSTThirdBodyDynamicContext(AuxiliaryElements aux, CelestialBody body, double[] parameters)	Constructor.
FieldDSSTThirdBodyDynamicContext(FieldAuxiliaryElements<T> aux, CelestialBody body, T[] parameters)	Constructor.