Get Satellite Orbital Elements by NORAD ID
celestrak.satellite.tleRetrieve current Two-Line Element (TLE) orbital data for a satellite by NORAD catalog number, including epoch, inclination, mean motion, and computed orbital period for tracking and pass predictions.
Instructions
Retrieve the current Two-Line Element (TLE) orbital data for a specific satellite using its NORAD catalog number. Returns the full GP (General Perturbations) element set: epoch, inclination, RAAN, eccentricity, argument of perigee, mean anomaly, mean motion (revolutions/day), B* drag coefficient, and computed orbital period in minutes. Data is sourced from the US Space Force 18th Space Control Squadron via CelesTrak. Useful for orbital mechanics calculations, satellite pass predictions, and tracking any of the 27,000+ catalogued space objects. Popular NORAD IDs: 25544 (ISS), 20580 (Hubble), 33591 (NOAA-18).
Input Schema
| Name | Required | Description | Default |
|---|---|---|---|
| catnr | Yes | NORAD catalog number (satellite ID). Examples: 25544 (ISS), 20580 (Hubble Space Telescope), 48274 (Starlink-1007). Integer between 1 and 99999. Obtain from celestrak.satellite.search or celestrak.satellite.group. |
Output Schema
| Name | Required | Description | Default |
|---|---|---|---|
| error | No | Present only when the call failed. Includes error code, message, request_id, and any provider-specific extras. | |
| result | No | Tool response payload. Shape varies per tool — consult the tool description and inputSchema. May be an object, array, string, or number depending on the upstream provider response. |