ClassicElementsMsgPayload

Typedefs

typedef ClassicElementsMsgPayload classicElements

struct ClassicElementsMsgPayload

#include <ClassicElementsMsgPayload.h>

Structure used to define classic orbit elements.

Public Members

double a: object semi-major axis

double e: Eccentricity of the orbit.

double i: inclination of the orbital plane

double Omega: Right ascension of the ascending node.

double omega: Argument of periapsis of the orbit.

double f: True anomaly of the orbit.

double rmag: Magnitude of the position vector (extra)

double alpha: Inverted semi-major axis (extra)

double rPeriap: Radius of periapsis (extra)

double rApoap: Radius if apoapsis (extra)