ae_orbit_t Struct Reference

For holding information on an orbit. More...

#include <aephem.h>

Data Fields
char	name [32]
	Name of the object.
double	epoch
	Epoch of orbital elements.
double	i
	Inclination, in degrees.
double	W
	Longitude of the ascending node, in degrees.
double	w
	Argument of the perihelion, in degrees.
double	a
	Mean distance (semimajor axis), in AU.
double	dm
	Daily motion, in AU per day.
double	ecc
	Eccentricity.
double	M
	Mean anomaly, in degrees.
double	equinox
	Epoch of equinox and ecliptic.
struct ae_plantbl_t *	ptable
	The perturbation tables.
double	L
	Computed mean longitude.
double	r
	Computed radius vector.
double	plat
	Perturbation in ecliptic latitude.

Detailed Description

For holding information on an orbit.

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

• aephem.h