Uses of Class
org.orekit.orbits.CircularOrbit

Packages that use CircularOrbit

Package	Description
org.orekit.orbits	This package provides classes to represent orbits.
org.orekit.propagation.analytical	Top level package for analytical propagators.

Uses of CircularOrbit in org.orekit.orbits

Methods in org.orekit.orbits that return CircularOrbit

Modifier and Type	Method	Description
CircularOrbit	CircularOrbitFactory.createFromDrivers()	Create orbital parameters from current drivers values.
CircularOrbit	CircularOrbit.inFrame(Frame inertialFrame)	Create a new object representing the same physical orbital state, but attached to a different reference frame.
CircularOrbit	CircularOrbit.shiftedBy(double dt)	Get a time-shifted orbit.
CircularOrbit	CircularOrbit.shiftedBy(TimeOffset dt)	Get a time-shifted orbit.
CircularOrbit	FieldCircularOrbit.toOrbit()	Transforms the FieldOrbit instance into an Orbit instance.
CircularOrbit	CircularOrbit.withCachedPositionAngleType(PositionAngleType positionAngleType)	Creates a new instance with the provided type used for caching.
CircularOrbit	CircularOrbit.withKeplerianRates()	Creates a new instance such that PositionAngleBased.hasNonKeplerianRates() is false.

Methods in org.orekit.orbits that return types with arguments of type CircularOrbit

Modifier and Type	Method	Description
AbstractOrbitFactory<CircularOrbit>	CircularOrbit.factory(PositionAngleType positionAngleType, double positionScale)	Get a factory for the current orbit type.

Constructors in org.orekit.orbits with parameters of type CircularOrbit

Modifier	Constructor	Description
	CircularOrbitFactory(CircularOrbit template, double positionScale, PositionAngleType positionAngleType)	Simple constructor.
	FieldCircularOrbit(Field<T> field, CircularOrbit op)	Constructor from Field and CircularOrbit.

Uses of CircularOrbit in org.orekit.propagation.analytical

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

Modifier and Type	Method	Description
static CircularOrbit	EcksteinHechlerPropagator.computeMeanOrbit(Orbit osculating, double referenceRadius, double mu, double c20, double c30, double c40, double c50, double c60, double epsilon, int maxIterations)	Conversion from osculating to mean orbit.
static CircularOrbit	EcksteinHechlerPropagator.computeMeanOrbit(Orbit osculating, double referenceRadius, double mu, double c20, double c30, double c40, double c50, double c60, OsculatingToMeanConverter converter)	Conversion from osculating to mean orbit.
static CircularOrbit	EcksteinHechlerPropagator.computeMeanOrbit(Orbit osculating, UnnormalizedSphericalHarmonicsProvider provider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics)	Conversion from osculating to mean orbit.
static CircularOrbit	EcksteinHechlerPropagator.computeMeanOrbit(Orbit osculating, UnnormalizedSphericalHarmonicsProvider provider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics, double epsilon, int maxIterations)	Conversion from osculating to mean orbit.
CircularOrbit	EcksteinHechlerPropagator.getOsculatingCircularOrbit(AbsoluteDate date)	Get the osculating circular orbit from the EH model.