Saylor Innovations Data Desk – Satellite Orbital Elements is a paid API for AI agents from saylorinnovations.com, paid per call via x402, $0.01/call, status unknown (last checked 2026-10-28).
Returns satellite orbital elements (epoch, inclination, eccentricity, period, perigee/apogee altitude, orbit class) from CelesTrak by NORAD catalog number
Satellite orbital elements from CelesTrak by NORAD id or name - epoch, inclination, eccentricity, period, perigee and apogee altitude and orbit class
A JSON object containing a 'satellites' array with full orbital element details for each matched satellite: name, NORAD ID, epoch timestamp, epoch age in hours, inclination in degrees, eccentricity, orbital period in minutes, perigee altitude in km, apogee altitude in km, semi-major axis in km, RAAN in degrees, argument of perigee in degrees, mean anomaly in degrees, B* drag term, and orbit class. Also includes the interpreted query, number of matches, data source attribution, and optional notes.
GEThttps://saylorinnovations.com/api/space/satellite?utm_source=zero.xyzChoose this endpoint when you need structured, parsed orbital element data (inclination, eccentricity, period, apogee/perigee, orbit class) for a specific satellite identified by NORAD catalog number, without needing to parse raw TLE text yourself. It is ideal for agents that need machine-readable orbital parameters for downstream calculations or display, rather than raw Two-Line Element sets. Prefer over raw CelesTrak if you want pre-computed altitude and period values.
| Field | Type | Description |
|---|---|---|
| inputrequired | object | |
| output | object |
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