Uses of Class
org.orekit.orbits.KeplerianOrbit

Packages that use KeplerianOrbit

Package	Description
org.orekit.estimation.iod	This package provides initial orbit determination methods.
org.orekit.files.ccsds	This package provides a parser for elements data stored in CCSDS Navigation Data Message format.
org.orekit.orbits	This package provides classes to represent orbits.

Uses of KeplerianOrbit in org.orekit.estimation.iod

Methods in org.orekit.estimation.iod that return KeplerianOrbit

Modifier and Type	Method and Description
KeplerianOrbit	IodLambert.estimate(Frame frame, boolean posigrade, int nRev, Vector3D p1, AbsoluteDate t1, Vector3D p2, AbsoluteDate t2) Estimate a Keplerian orbit given two position vectors and a duration.
KeplerianOrbit	IodGibbs.estimate(Frame frame, PV pv1, PV pv2, PV pv3) Give an initial orbit estimation, assuming Keplerian motion.
KeplerianOrbit	IodGibbs.estimate(Frame frame, Vector3D r1, AbsoluteDate date1, Vector3D r2, AbsoluteDate date2, Vector3D r3, AbsoluteDate date3) Give an initial orbit estimation, assuming Keplerian motion.
KeplerianOrbit	IodGooding.estimate(Vector3D O1, Vector3D O2, Vector3D O3, Vector3D lineOfSight1, AbsoluteDate dateObs1, Vector3D lineOfSight2, AbsoluteDate dateObs2, Vector3D lineOfSight3, AbsoluteDate dateObs3, double rho1init, double rho3init) Orbit got from Observed Three Lines of Sight (angles only).
KeplerianOrbit	IodGooding.estimate(Vector3D O1, Vector3D O2, Vector3D O3, Vector3D lineOfSight1, AbsoluteDate dateObs1, Vector3D lineOfSight2, AbsoluteDate dateObs2, Vector3D lineOfSight3, AbsoluteDate dateObs3, double rho1init, double rho3init, int nRev, boolean direction) Orbit got from Observed Three Lines of Sight (angles only).

Uses of KeplerianOrbit in org.orekit.files.ccsds

Methods in org.orekit.files.ccsds that return KeplerianOrbit

Modifier and Type	Method and Description
KeplerianOrbit	OMMFile.generateKeplerianOrbit() Generate a KeplerianOrbit based on the OMM mean Keplerian elements.
KeplerianOrbit	OPMFile.generateKeplerianOrbit() Generate a KeplerianOrbit from the OPM Keplerian elements if hasKeplerianElements is true, or from the state vector data otherwise.

Uses of KeplerianOrbit in org.orekit.orbits

Methods in org.orekit.orbits that return KeplerianOrbit

Modifier and Type	Method and Description
KeplerianOrbit	KeplerianOrbit.interpolate(AbsoluteDate date, Stream<Orbit> sample) Get an interpolated instance.
KeplerianOrbit	KeplerianOrbit.shiftedBy(double dt) Get a time-shifted orbit.
KeplerianOrbit	FieldKeplerianOrbit.toOrbit()