Uses of Interface
org.orekit.propagation.Propagator

Packages that use Propagator

Package	Description
org.orekit.attitudes	This package provides classes to represent simple attitudes.
org.orekit.propagation	This package provides tools to propagate orbital states with different methods.
org.orekit.propagation.analytical
org.orekit.propagation.analytical.tle	This package provides classes to read and extrapolate tle's.
org.orekit.propagation.conversion	This package provides tools to convert a given propagator or a set of SpacecraftState into another propagator.
org.orekit.propagation.integration
org.orekit.propagation.numerical
org.orekit.propagation.semianalytical.dsst	This package provides an implementation of the Draper Semi-analytical Satellite Theory (DSST).

Uses of Propagator in org.orekit.attitudes

Methods in org.orekit.attitudes with parameters of type Propagator

Modifier and Type	Method and Description
void	AttitudesSequence.registerSwitchEvents(Propagator propagator) Register all wrapped switch events to the propagator.

Uses of Propagator in org.orekit.propagation

Subinterfaces of Propagator in org.orekit.propagation

Modifier and Type	Interface and Description
interface	BoundedPropagator This interface is intended for ephemerides valid only during a time range.

Classes in org.orekit.propagation that implement Propagator

Modifier and Type	Class and Description
class	AbstractPropagator Common handling of Propagator methods for analytical propagators.

Uses of Propagator in org.orekit.propagation.analytical

Classes in org.orekit.propagation.analytical that implement Propagator

Modifier and Type	Class and Description
class	AbstractAnalyticalPropagator Common handling of Propagator methods for analytical propagators.
class	AdapterPropagator Orbit propagator that adapts an underlying propagator, adding differential effects.
class	EcksteinHechlerPropagator This class propagates a SpacecraftState using the analytical Eckstein-Hechler model.
class	Ephemeris This class is designed to accept and handle tabulated orbital entries.
class	KeplerianPropagator Simple keplerian orbit propagator.

Methods in org.orekit.propagation.analytical that return Propagator

Modifier and Type	Method and Description
Propagator	AdapterPropagator.getPropagator() Get the reference propagator.

Constructors in org.orekit.propagation.analytical with parameters of type Propagator

Constructor and Description
AdapterPropagator(Propagator reference) Build a propagator from an underlying reference propagator.

Uses of Propagator in org.orekit.propagation.analytical.tle

Classes in org.orekit.propagation.analytical.tle that implement Propagator

Modifier and Type	Class and Description
class	TLEPropagator This class provides elements to propagate TLE's.

Uses of Propagator in org.orekit.propagation.conversion

Methods in org.orekit.propagation.conversion that return Propagator

Modifier and Type	Method and Description
Propagator	PropagatorBuilder.buildPropagator(AbsoluteDate date, double[] parameters) Build a propagator.
Propagator	TLEPropagatorBuilder.buildPropagator(AbsoluteDate date, double[] parameters) Build a propagator.
Propagator	KeplerianPropagatorBuilder.buildPropagator(AbsoluteDate date, double[] parameters) Build a propagator.
Propagator	EcksteinHechlerPropagatorBuilder.buildPropagator(AbsoluteDate date, double[] parameters) Build a propagator.
Propagator	AbstractPropagatorConverter.convert(List<SpacecraftState> states, boolean positionOnly, Collection<String> freeParameters) Find the propagator that minimize the mean square error for a sample of states.
Propagator	PropagatorConverter.convert(List<SpacecraftState> states, boolean positionOnly, Collection<String> freeParameters) Find the propagator that minimize the mean square error for a sample of states.
Propagator	AbstractPropagatorConverter.convert(List<SpacecraftState> states, boolean positionOnly, String... freeParameters) Find the propagator that minimize the mean square error for a sample of states.
Propagator	PropagatorConverter.convert(List<SpacecraftState> states, boolean positionOnly, String... freeParameters) Find the propagator that minimize the mean square error for a sample of states.
Propagator	AbstractPropagatorConverter.convert(Propagator source, double timeSpan, int nbPoints, Collection<String> freeParameters) Convert a propagator to another.
Propagator	PropagatorConverter.convert(Propagator source, double timeSpan, int nbPoints, Collection<String> freeParameters) Convert a propagator into another one.
Propagator	AbstractPropagatorConverter.convert(Propagator source, double timeSpan, int nbPoints, String... freeParameters) Convert a propagator to another.
Propagator	PropagatorConverter.convert(Propagator source, double timeSpan, int nbPoints, String... freeParameters) Convert a propagator into another one.
Propagator	AbstractPropagatorConverter.getAdaptedPropagator() Get the adapted propagator.

Methods in org.orekit.propagation.conversion with parameters of type Propagator

Modifier and Type	Method and Description
Propagator	AbstractPropagatorConverter.convert(Propagator source, double timeSpan, int nbPoints, Collection<String> freeParameters) Convert a propagator to another.
Propagator	PropagatorConverter.convert(Propagator source, double timeSpan, int nbPoints, Collection<String> freeParameters) Convert a propagator into another one.
Propagator	AbstractPropagatorConverter.convert(Propagator source, double timeSpan, int nbPoints, String... freeParameters) Convert a propagator to another.
Propagator	PropagatorConverter.convert(Propagator source, double timeSpan, int nbPoints, String... freeParameters) Convert a propagator into another one.

Constructors in org.orekit.propagation.conversion with parameters of type Propagator

Constructor and Description
OsculatingToMeanElementsConverter(SpacecraftState state, int satelliteRevolution, Propagator propagator) Constructor.

Uses of Propagator in org.orekit.propagation.integration

Classes in org.orekit.propagation.integration that implement Propagator

Modifier and Type	Class and Description
class	AbstractIntegratedPropagator Common handling of Propagator methods for both numerical and semi-analytical propagators.
class	IntegratedEphemeris This class stores sequentially generated orbital parameters for later retrieval.

Uses of Propagator in org.orekit.propagation.numerical

Classes in org.orekit.propagation.numerical that implement Propagator

Modifier and Type	Class and Description
class	NumericalPropagator This class propagates orbits using numerical integration.

Uses of Propagator in org.orekit.propagation.semianalytical.dsst

Classes in org.orekit.propagation.semianalytical.dsst that implement Propagator

Modifier and Type	Class and Description
class	DSSTPropagator This class propagates orbits using the DSST theory.