Orbit
perigee_orbitOrbit of an object: perigee and apogee altitudes (periapsis/apoapsis), period, inclination, eccentricity, semi-major axis. Earth satellites: the mean elements of their published element set, with the orbit regime (LEO, MEO, GEO, HEO); other objects: instantaneous two-body elements around their centre at a date (default: the body they orbit; inclination on its equator, on the ecliptic around the Sun).
Input Schema
| Name | Required | Description | Default |
|---|---|---|---|
| id | Yes | ||
| date | No | ISO 8601 UTC instant, e.g. 2026-12-01T00:00:00Z (default: now). | |
| centre | No | Body the orbit is around, e.g. "sun" for a planet or a probe. |