pylupnt.EphemerisOrbitConfig

class pylupnt.EphemerisOrbitConfig

Initial classical orbital elements for the study’s truth trajectory.

property a_m

Semi-major axis [m].

property argp_rad

Argument of periapsis [rad].

property coe_frame

Frame the elements are defined in (e.g. MOON_OP).

property ecc

Eccentricity.

property inc_rad

Inclination [rad].

property m0_rad

Initial mean anomaly [rad].

property raan_rad

Right ascension of the ascending node [rad].