OrbitalElements Class Reference

The extracted orbital elements used by the SGP4 propagator. More...

#include <OrbitalElements.h>

Collaboration diagram for OrbitalElements:

Public Member Functions
	OrbitalElements (const Tle &tle)
double	MeanAnomoly () const
double	AscendingNode () const
double	ArgumentPerigee () const
double	Eccentricity () const
double	Inclination () const
double	MeanMotion () const
double	BStar () const
double	RecoveredSemiMajorAxis () const
double	RecoveredMeanMotion () const
double	Perigee () const
double	Period () const
DateTime	Epoch () const

Private Attributes
double	mean_anomoly_
double	ascending_node_
double	argument_perigee_
double	eccentricity_
double	inclination_
double	mean_motion_
double	bstar_
double	recovered_semi_major_axis_
double	recovered_mean_motion_
double	perigee_
double	period_
DateTime	epoch_

Detailed Description

The extracted orbital elements used by the SGP4 propagator.

Constructor & Destructor Documentation

OrbitalElements::OrbitalElements

(

const Tle &

tle

)

Member Function Documentation

double OrbitalElements::ArgumentPerigee ( ) const

inline

double OrbitalElements::AscendingNode ( ) const

inline

double OrbitalElements::BStar ( ) const

inline

double OrbitalElements::Eccentricity ( ) const

inline

DateTime OrbitalElements::Epoch ( ) const

inline

double OrbitalElements::Inclination ( ) const

inline

double OrbitalElements::MeanAnomoly ( ) const

inline

double OrbitalElements::MeanMotion ( ) const

inline

double OrbitalElements::Perigee ( ) const

inline

double OrbitalElements::Period ( ) const

inline

double OrbitalElements::RecoveredMeanMotion ( ) const

inline

double OrbitalElements::RecoveredSemiMajorAxis ( ) const

inline

Member Data Documentation

double OrbitalElements::argument_perigee_

private

double OrbitalElements::ascending_node_

private

double OrbitalElements::bstar_

private

double OrbitalElements::eccentricity_

private

DateTime OrbitalElements::epoch_

private

double OrbitalElements::inclination_

private

double OrbitalElements::mean_anomoly_

private

double OrbitalElements::mean_motion_

private

double OrbitalElements::perigee_

private

double OrbitalElements::period_

private

double OrbitalElements::recovered_mean_motion_

private

double OrbitalElements::recovered_semi_major_axis_

private

---

The documentation for this class was generated from the following file:

• /home/travis/build/TUW-VieVS/VieSchedpp/SGP4/OrbitalElements.h