ClassicElementsMsgPayload

struct ClassicElementsMsgPayload

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)