Uses of Class
org.orekit.propagation.conversion.averaging.elements.AveragedKeplerianWithMeanAngle

Packages that use AveragedKeplerianWithMeanAngle

Package	Description
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.

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

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

Modifier and Type	Method	Description
AveragedKeplerianWithMeanAngle	BrouwerLyddaneOrbitalState.getAveragedElements()	Getter for the averaged orbital elements.
AveragedKeplerianWithMeanAngle	SGP4OrbitalState.getAveragedElements()	Getter for the averaged orbital elements.

Constructors in org.orekit.propagation.conversion.averaging with parameters of type AveragedKeplerianWithMeanAngle

Modifier	Constructor	Description
	BrouwerLyddaneOrbitalState(AbsoluteDate date, AveragedKeplerianWithMeanAngle elements, Frame frame, UnnormalizedSphericalHarmonicsProvider harmonicsProvider)	Constructor.
	SGP4OrbitalState(AbsoluteDate date, AveragedKeplerianWithMeanAngle elements)	Constructor with default data context.
	SGP4OrbitalState(AbsoluteDate date, AveragedKeplerianWithMeanAngle elements, DataContext dataContext)	Constructor.