Part VI. Orbit properties
Table of Contents
- CL_kp_E2M — Eccentric anomaly to mean anomaly for elliptic and hyperbolic orbits
- CL_kp_E2v — Eccentric anomaly to true anomaly
- CL_kp_M2E — Solution of kepler's equation (ecc,M to E)
- CL_kp_M2Egene — Solution of generalized kepler's equation (ex, ey, M to E)
- CL_kp_M2v — True anomaly to mean anomaly
- CL_kp_characteristics — Various Keplerian characteristics
- CL_kp_params — Orbit properties with a Keplerian motion (mean motion, period, longitude gap between 2 orbits)
- CL_kp_v2E — True anomaly to eccentric anomaly
- CL_kp_v2M — True anomaly to mean anomaly
- CL_op_driftJ2 — Drift of orbital elements due to J2
- CL_op_frozenOrbit — Eccentricity and perigee argument for a frozen orbit
- CL_op_frozenOrbitDer — Eccentricity and perigee drift over time for an orbit close to a frozen orbit
- CL_op_locTime — Local time or right ascension at date
- CL_op_paramsJ2 — Orbit properties including J2 effects (mean motion, period, nodal period, longitude gap between 2 orbits)
- CL_op_rarp2ae — Apoapsis radius and periapsis radius to semi major axis and eccentricity (elliptic orbits)
- CL_op_rava2ae — Apoapsis radius and velocity to semi major axis and eccentricity (elliptic orbits)
- CL_op_repeat2smaInc — Repeat orbit parameters (N,P,Q) to semi major axis and inclination
- CL_op_repeatGroundTracks — Longitudes of repeating ground tracks
- CL_op_rpvinf2ae — Periapsis radius and velocity at infinity to semi major axis and eccentricity (hyperbolic orbits)
- CL_op_rpvp2ae — Periapsis radius and velocity at periapsis to semi major axis and eccentricity
- CL_op_searchRepeatOrbits — Search for repeat orbits
- CL_op_ssoJ2 — Semi major axis, eccentricity or inclination for a sun synchronous orbit (J2)