Uses of Class
org.orekit.orbits.OrbitType

Packages that use OrbitType

Package	Description
org.orekit.forces.maneuvers	This package provides models of simple maneuvers.
org.orekit.orbits	This package provides classes to represent orbits.
org.orekit.propagation	Propagation
org.orekit.propagation.analytical	Top level package for analytical propagators.
org.orekit.propagation.conversion	This package provides tools to convert a given propagator or a set of SpacecraftState into another propagator.
org.orekit.propagation.conversion.averaging	This package wraps methods from various (semi)analytical models in Orekit to convert back and forth between an averaged orbital state and an osculating one.
org.orekit.propagation.events	This package provides interfaces and classes dealing with events occurring during propagation.
org.orekit.propagation.integration	Utilities for integration-based propagators (both numerical and semi-analytical).
org.orekit.propagation.numerical	Top level package for numerical propagators.
org.orekit.propagation.semianalytical.dsst	This package provides an implementation of the Draper Semi-analytical Satellite Theory (DSST).
org.orekit.utils	This package provides useful objects.

Uses of OrbitType in org.orekit.forces.maneuvers

Constructors in org.orekit.forces.maneuvers with parameters of type OrbitType

Constructor	Description
SmallManeuverAnalyticalModel(SpacecraftState state0, OrbitType orbitType, Vector3D dV, double isp)	Build a maneuver defined in spacecraft frame.
SmallManeuverAnalyticalModel(SpacecraftState state0, OrbitType orbitType, Frame frame, Vector3D dV, double isp)	Build a maneuver defined in user-specified frame.

Uses of OrbitType in org.orekit.orbits

Methods in org.orekit.orbits that return OrbitType

Modifier and Type	Method	Description
OrbitType	CartesianOrbit.getType()	Get the orbit type.
OrbitType	CircularOrbit.getType()	Get the orbit type.
OrbitType	EquinoctialOrbit.getType()	Get the orbit type.
OrbitType	FieldCartesianOrbit.getType()	Get the orbit type.
OrbitType	FieldCircularOrbit.getType()	Get the orbit type.
OrbitType	FieldEquinoctialOrbit.getType()	Get the orbit type.
OrbitType	FieldKeplerianOrbit.getType()	Get the orbit type.
abstract OrbitType	FieldOrbit.getType()	Get the orbit type.
OrbitType	KeplerianOrbit.getType()	Get the orbit type.
abstract OrbitType	Orbit.getType()	Get the orbit type.
static OrbitType	OrbitType.valueOf(String name)	Returns the enum constant of this type with the specified name.
static OrbitType[]	OrbitType.values()	Returns an array containing the constants of this enum type, in the order they are declared.

Uses of OrbitType in org.orekit.propagation

Methods in org.orekit.propagation that return OrbitType

Modifier and Type	Method	Description
OrbitType	StateCovarianceMatrixProvider.getCovarianceOrbitType()	Get the orbit type in which the covariance matrix is expressed.
OrbitType	FieldStateCovariance.getOrbitType()	Get the covariance orbit type.
OrbitType	MatricesHarvester.getOrbitType()	Get the orbit type used for the matrix computation.
OrbitType	StateCovariance.getOrbitType()	Get the covariance orbit type.
OrbitType	AbstractStateCovarianceInterpolator.getOutOrbitType()	Get output orbit type.

Methods in org.orekit.propagation with parameters of type OrbitType

Modifier and Type	Method	Description
FieldStateCovariance<T>	FieldStateCovariance.changeCovarianceType(FieldOrbit<T> orbit, OrbitType outOrbitType, PositionAngleType outAngleType)	Get the covariance matrix in another orbit type.
StateCovariance	StateCovariance.changeCovarianceType(Orbit orbit, OrbitType outOrbitType, PositionAngleType outAngleType)	Get the covariance matrix in another orbit type.
static void	StateCovariance.checkFrameAndOrbitTypeConsistency(Frame covarianceFrame, OrbitType inputType)	Check constructor's inputs consistency.
StateCovariance	StateCovarianceMatrixProvider.getStateCovariance(SpacecraftState state, OrbitType orbitType, PositionAngleType angleType)	Get the state covariance expressed in a given orbit type.
default <T extends CalculusFieldElement<T>> double[][]	ToleranceProvider.getTolerances(FieldOrbit<T> referenceOrbit, OrbitType propagationOrbitType)	Retrieve the integration tolerances given a reference Field orbit.
default <T extends CalculusFieldElement<T>> double[][]	ToleranceProvider.getTolerances(FieldOrbit<T> referenceOrbit, OrbitType propagationOrbitType, PositionAngleType positionAngleType)	Retrieve the integration tolerances given a reference Field orbit.
default double[][]	ToleranceProvider.getTolerances(Orbit referenceOrbit, OrbitType propagationOrbitType)	Retrieve the integration tolerances given a reference orbit.
double[][]	ToleranceProvider.getTolerances(Orbit referenceOrbit, OrbitType propagationOrbitType, PositionAngleType positionAngleType)	Retrieve the integration tolerances given a reference orbit.
static boolean	StateCovariance.inputAndOutputAreIdentical(OrbitType inOrbitType, PositionAngleType inAngleType, OrbitType outOrbitType, PositionAngleType outAngleType)	Checks if input/output orbit and angle types are identical.
static boolean	StateCovariance.inputAndOutputOrbitTypesAreCartesian(OrbitType inOrbitType, OrbitType outOrbitType)	Checks if input and output orbit types are both OrbitType.CARTESIAN.

Constructors in org.orekit.propagation with parameters of type OrbitType

Constructor	Description
AbstractStateCovarianceInterpolator(int interpolationPoints, double extrapolationThreshold, TimeInterpolator<Orbit> orbitInterpolator, Frame outFrame, OrbitType outOrbitType, PositionAngleType outPositionAngleType)	Constructor.
FieldStateCovariance(FieldMatrix<T> orbitalCovariance, FieldAbsoluteDate<T> epoch, Frame covarianceFrame, OrbitType orbitType, PositionAngleType angleType)	Constructor.
StateCovariance(RealMatrix orbitalCovariance, AbsoluteDate epoch, Frame covarianceFrame, OrbitType orbitType, PositionAngleType angleType)	Constructor.
StateCovarianceBlender(SmoothStepFactory.SmoothStepFunction blendingFunction, TimeInterpolator<Orbit> orbitInterpolator, Frame outFrame, OrbitType outOrbitType, PositionAngleType outPositionAngleType)	Constructor.
StateCovarianceKeplerianHermiteInterpolator(int interpolationPoints, double extrapolationThreshold, TimeInterpolator<Orbit> orbitInterpolator, CartesianDerivativesFilter filter, Frame outFrame, OrbitType outOrbitType, PositionAngleType outPositionAngleType)	Constructor using an output frame.
StateCovarianceKeplerianHermiteInterpolator(int interpolationPoints, TimeInterpolator<Orbit> orbitInterpolator, Frame outFrame, OrbitType outOrbitType, PositionAngleType outPositionAngleType)	Constructor using an output frame and : Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Use of position and two time derivatives during interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
StateCovarianceKeplerianHermiteInterpolator(int interpolationPoints, TimeInterpolator<Orbit> orbitInterpolator, CartesianDerivativesFilter filter, Frame outFrame, OrbitType outOrbitType, PositionAngleType outPositionAngleType)	Constructor using an output frame and : Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
StateCovarianceKeplerianHermiteInterpolator(TimeInterpolator<Orbit> orbitInterpolator, Frame outFrame, OrbitType outOrbitType, PositionAngleType outPositionAngleType)	Constructor using an output frame and : Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of position and two time derivatives during interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).

Uses of OrbitType in org.orekit.propagation.analytical

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

Modifier and Type	Method	Description
OrbitType	AbstractAnalyticalMatricesHarvester.getOrbitType()	Get the orbit type used for the matrix computation.

Uses of OrbitType in org.orekit.propagation.conversion

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

Modifier and Type	Method	Description
OrbitType	AbstractPropagatorBuilder.getOrbitType()	Get the orbit type expected for the 6 first parameters in PropagatorBuilder.buildPropagator(double[]).
OrbitType	PropagatorBuilder.getOrbitType()	Get the orbit type expected for the 6 first parameters in PropagatorBuilder.buildPropagator(double[]).

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

Modifier and Type	Method	Description
T	AbstractIntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType)
abstract T	AbstractIntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType, PositionAngleType angleType)
W	AbstractVariableStepFieldIntegratorBuilder.buildIntegrator(Field<T> field, Orbit orbit, OrbitType orbitType, PositionAngleType angleType)	Build a first order integrator.
T	AbstractVariableStepIntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType, PositionAngleType angleType)	Build a first order integrator.
ClassicalRungeKuttaFieldIntegrator<T>	ClassicalRungeKuttaFieldIntegratorBuilder.buildIntegrator(Field<T> field, Orbit orbit, OrbitType orbitType, PositionAngleType angleType)	Build a first order integrator.
ClassicalRungeKuttaIntegrator	ClassicalRungeKuttaIntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType, PositionAngleType angleType)	Build a first order integrator.
EulerFieldIntegrator<T>	EulerFieldIntegratorBuilder.buildIntegrator(Field<T> field, Orbit orbit, OrbitType orbitType, PositionAngleType angleType)	Build a first order integrator.
EulerIntegrator	EulerIntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType, PositionAngleType angleType)	Build a first order integrator.
ExplicitRungeKuttaIntegrator	ExplicitRungeKuttaIntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType)	Build a first order integrator.
ExplicitRungeKuttaIntegrator	ExplicitRungeKuttaIntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType, PositionAngleType angleType)	Build a first order integrator.
W	FieldAbstractIntegratorBuilder.buildIntegrator(Field<T> field, Orbit orbit, OrbitType orbitType)	Build a first order integrator.
abstract W	FieldAbstractIntegratorBuilder.buildIntegrator(Field<T> field, Orbit orbit, OrbitType orbitType, PositionAngleType angleType)	Build a first order integrator.
W	FieldAbstractIntegratorBuilder.buildIntegrator(FieldOrbit<T> orbit, OrbitType orbitType)	Build a first order integrator.
FieldExplicitRungeKuttaIntegrator<T>	FieldExplicitRungeKuttaIntegratorBuilder.buildIntegrator(Field<T> field, Orbit orbit, OrbitType orbitType)	Build a first order integrator.
FieldExplicitRungeKuttaIntegrator<T>	FieldExplicitRungeKuttaIntegratorBuilder.buildIntegrator(Field<T> field, Orbit orbit, OrbitType orbitType, PositionAngleType angleType)	Build a first order integrator.
FieldExplicitRungeKuttaIntegrator<T>	FieldExplicitRungeKuttaIntegratorBuilder.buildIntegrator(FieldOrbit<T> orbit, OrbitType orbitType)	Build a first order integrator.
FieldODEIntegrator<T>	FieldODEIntegratorBuilder.buildIntegrator(Field<T> field, Orbit orbit, OrbitType orbitType)	Build a first order integrator.
FieldODEIntegrator<T>	FieldODEIntegratorBuilder.buildIntegrator(Field<T> field, Orbit orbit, OrbitType orbitType, PositionAngleType angleType)	Build a first order integrator.
FieldODEIntegrator<T>	FieldODEIntegratorBuilder.buildIntegrator(FieldOrbit<T> orbit, OrbitType orbitType)	Build a first order integrator.
GillFieldIntegrator<T>	GillFieldIntegratorBuilder.buildIntegrator(Field<T> field, Orbit orbit, OrbitType orbitType, PositionAngleType angleType)	Build a first order integrator.
GillIntegrator	GillIntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType, PositionAngleType angleType)	Build a first order integrator.
LutherFieldIntegrator<T>	LutherFieldIntegratorBuilder.buildIntegrator(Field<T> field, Orbit orbit, OrbitType orbitType, PositionAngleType positionAngleType)	Build a first order integrator.
LutherIntegrator	LutherIntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType, PositionAngleType angleType)	Build a first order integrator.
MidpointFieldIntegrator<T>	MidpointFieldIntegratorBuilder.buildIntegrator(Field<T> field, Orbit orbit, OrbitType orbitType, PositionAngleType angleType)	Build a first order integrator.
MidpointIntegrator	MidpointIntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType, PositionAngleType angleType)	Build a first order integrator.
ODEIntegrator	ODEIntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType)	Build a first order integrator.
ODEIntegrator	ODEIntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType, PositionAngleType angleType)	Build a first order integrator.
ThreeEighthesFieldIntegrator<T>	ThreeEighthesFieldIntegratorBuilder.buildIntegrator(Field<T> field, Orbit orbit, OrbitType orbitType, PositionAngleType angleType)	Build a first order integrator.
ThreeEighthesIntegrator	ThreeEighthesIntegratorBuilder.buildIntegrator(Orbit orbit, OrbitType orbitType, PositionAngleType angleType)	Build a first order integrator.
protected double[][]	AbstractVariableStepFieldIntegratorBuilder.getTolerances(Orbit orbit, OrbitType orbitType, PositionAngleType angleType)	Computes tolerances.
protected double[][]	AbstractVariableStepIntegratorBuilder.getTolerances(Orbit orbit, OrbitType orbitType)	Computes tolerances.

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

Constructor	Description
BrouwerLyddanePropagatorBuilder(Orbit templateOrbit, double referenceRadius, double mu, TideSystem tideSystem, double c20, double c30, double c40, double c50, OrbitType orbitType, PositionAngleType positionAngleType, double positionScale, double M2)	Build a new instance.
EcksteinHechlerPropagatorBuilder(Orbit templateOrbit, double referenceRadius, double mu, TideSystem tideSystem, double c20, double c30, double c40, double c50, double c60, OrbitType orbitType, PositionAngleType positionAngleType, double positionScale)	Build a new instance.

Uses of OrbitType in org.orekit.propagation.conversion.averaging

Methods in org.orekit.propagation.conversion.averaging that return OrbitType

Modifier and Type	Method	Description
OrbitType	AveragedOrbitalState.getOrbitType()	Getter for the averaged orbit type.
OrbitType	BrouwerLyddaneOrbitalState.getOrbitType()	Getter for the averaged orbit type.
OrbitType	DSST6X0OrbitalState.getOrbitType()	Getter for the averaged orbit type.
OrbitType	EcksteinHechlerOrbitalState.getOrbitType()	Getter for the averaged orbit type.
OrbitType	SGP4OrbitalState.getOrbitType()	Getter for the averaged orbit type.

Uses of OrbitType in org.orekit.propagation.events

Methods in org.orekit.propagation.events that return OrbitType

Modifier and Type	Method	Description
OrbitType	PositionAngleDetector.getOrbitType()	Get the orbit type defining the angle type.

Constructors in org.orekit.propagation.events with parameters of type OrbitType

Constructor	Description
PositionAngleDetector(double maxCheck, double threshold, OrbitType orbitType, PositionAngleType positionAngleType, double angle)	Build a detector.
PositionAngleDetector(OrbitType orbitType, PositionAngleType positionAngleType, double angle)	Build a new detector.
PositionAngleDetector(EventDetectionSettings detectionSettings, EventHandler handler, OrbitType orbitType, PositionAngleType positionAngleType, double angle)	Protected constructor with full parameters.

Uses of OrbitType in org.orekit.propagation.integration

Methods in org.orekit.propagation.integration that return OrbitType

Modifier and Type	Method	Description
protected OrbitType	AbstractIntegratedPropagator.getOrbitType()	Get propagation parameter type.
protected OrbitType	FieldAbstractIntegratedPropagator.getOrbitType()	Get propagation parameter type.
OrbitType	FieldStateMapper.getOrbitType()	Get propagation parameter type.
OrbitType	StateMapper.getOrbitType()	Get propagation parameter type.

Methods in org.orekit.propagation.integration with parameters of type OrbitType

Modifier and Type	Method	Description
protected abstract StateMapper	AbstractIntegratedPropagator.createMapper(AbsoluteDate referenceDate, double mu, OrbitType orbitType, PositionAngleType positionAngleType, AttitudeProvider attitudeProvider, Frame frame)	Create a mapper between raw double components and spacecraft state. /** Simple constructor.
protected abstract FieldStateMapper<T>	FieldAbstractIntegratedPropagator.createMapper(FieldAbsoluteDate<T> referenceDate, T mu, OrbitType orbitType, PositionAngleType positionAngleType, AttitudeProvider attitudeProvider, Frame frame)	Create a mapper between raw double components and spacecraft state. /** Simple constructor.
protected void	AbstractIntegratedPropagator.setOrbitType(OrbitType orbitType)	Set propagation orbit type.
protected void	FieldAbstractIntegratedPropagator.setOrbitType(OrbitType orbitType)	Set propagation orbit type.

Constructors in org.orekit.propagation.integration with parameters of type OrbitType

Constructor	Description
FieldStateMapper(FieldAbsoluteDate<T> referenceDate, T mu, OrbitType orbitType, PositionAngleType positionAngleType, AttitudeProvider attitudeProvider, Frame frame)	Simple constructor.
StateMapper(AbsoluteDate referenceDate, double mu, OrbitType orbitType, PositionAngleType positionAngleType, AttitudeProvider attitudeProvider, Frame frame)	Simple constructor.

Uses of OrbitType in org.orekit.propagation.numerical

Fields in org.orekit.propagation.numerical declared as OrbitType

Modifier and Type	Field	Description
static OrbitType	NumericalPropagator.DEFAULT_ORBIT_TYPE	Default orbit type.

Methods in org.orekit.propagation.numerical that return OrbitType

Modifier and Type	Method	Description
OrbitType	FieldNumericalPropagator.getOrbitType()	Get propagation parameter type.
OrbitType	NumericalPropagator.getOrbitType()	Get propagation parameter type.

Methods in org.orekit.propagation.numerical with parameters of type OrbitType

Modifier and Type	Method	Description
protected FieldStateMapper<T>	FieldNumericalPropagator.createMapper(FieldAbsoluteDate<T> referenceDate, T mu, OrbitType orbitType, PositionAngleType positionAngleType, AttitudeProvider attitudeProvider, Frame frame)	Create a mapper between raw double components and spacecraft state. /** Simple constructor.
protected StateMapper	GLONASSNumericalPropagator.createMapper(AbsoluteDate referenceDate, double mu, OrbitType orbitType, PositionAngleType positionAngleType, AttitudeProvider attitudeProvider, Frame frame)
protected StateMapper	NumericalPropagator.createMapper(AbsoluteDate referenceDate, double mu, OrbitType orbitType, PositionAngleType positionAngleType, AttitudeProvider attitudeProvider, Frame frame)	Create a mapper between raw double components and spacecraft state. /** Simple constructor.
void	FieldNumericalPropagator.setOrbitType(OrbitType orbitType)	Set propagation orbit type.
void	NumericalPropagator.setOrbitType(OrbitType orbitType)	Set propagation orbit type.
static <T extends CalculusFieldElement<T>> double[][]	FieldNumericalPropagator.tolerances(T dP, FieldOrbit<T> orbit, OrbitType type)	Deprecated. since 13.0.
static <T extends CalculusFieldElement<T>> double[][]	FieldNumericalPropagator.tolerances(T dP, T dV, FieldOrbit<T> orbit, OrbitType type)	Deprecated. since 13.0.
static double[][]	NumericalPropagator.tolerances(double dP, double dV, Orbit orbit, OrbitType type)	Deprecated. since 13.0.
static double[][]	NumericalPropagator.tolerances(double dP, Orbit orbit, OrbitType type)	Deprecated. since 13.0.

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

Methods in org.orekit.propagation.semianalytical.dsst that return OrbitType

Modifier and Type	Method	Description
OrbitType	DSSTHarvester.getOrbitType()	Get the orbit type used for the matrix computation.
OrbitType	DSSTPropagator.getOrbitType()	Get propagation parameter type.
OrbitType	FieldDSSTPropagator.getOrbitType()	Get propagation parameter type.

Methods in org.orekit.propagation.semianalytical.dsst with parameters of type OrbitType

Modifier and Type	Method	Description
protected StateMapper	DSSTPropagator.createMapper(AbsoluteDate referenceDate, double mu, OrbitType ignoredOrbitType, PositionAngleType ignoredPositionAngleType, AttitudeProvider attitudeProvider, Frame frame)	Create a mapper between raw double components and spacecraft state. /** Simple constructor.
protected FieldStateMapper<T>	FieldDSSTPropagator.createMapper(FieldAbsoluteDate<T> referenceDate, T mu, OrbitType ignoredOrbitType, PositionAngleType ignoredPositionAngleType, AttitudeProvider attitudeProvider, Frame frame)	Create a mapper between raw double components and spacecraft state. /** Simple constructor.

Uses of OrbitType in org.orekit.utils

Methods in org.orekit.utils with parameters of type OrbitType

Modifier and Type	Method	Description
static StateJacobian	Differentiation.differentiate(StateFunction function, int dimension, AttitudeProvider provider, OrbitType orbitType, PositionAngleType positionAngleType, double dP, int nbPoints)	Differentiate a vector function using finite differences.