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).
Tool call template
Replace each placeholder with a value matching the input schema. Only required parameters are included; add optional parameters as needed.
{
"id": 1,
"jsonrpc": "2.0",
"method": "tools/call",
"params": {
"arguments": {
"id": "<id>"
},
"name": "perigee_orbit"
}
}Input Schema
| Name | Required | Description | Default |
|---|---|---|---|
| id | Yes | Object id from perigee_find (NORAD number, mission id, planet, "moon:<id>", "site:<id>", "launch:<id>", "star:<id>", "comet:<id>", "asteroid:<id>" or a dwarf planet name), e.g. "25544" for the ISS. | |
| 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. |