THEMIS A — Live Satellite Tracking (NORAD 30580)
Track THEMIS A (NORAD Catalog Number 30580) live on the WatchSat interactive 3D globe. Its orbital position is propagated in real time from CelesTrak TLE data using the SGP4/SDP4 model.
Orbital elements (from latest TLE)
- Orbit regime: low Earth orbit (LEO)
- Perigee × apogee altitude: 1182 km × 78183 km
- Inclination: 8.67°
- Orbital period: 1639.3 minutes (0.88 revolutions/day)
- Eccentricity: 0.83600
- Element set epoch: 2026-07-10