Satellites/ICEYE-X82
ICEYE-X82
Satellite · FinlandActive
Who
Owner / operatorICEYE
ManufacturerICEYE
CountryFinland
Catalogue owner codePOR
Orbit
OrbitingEarth
Orbit classLEO
Perigee588 km
Apogee596 km
Inclination97.72°
Period96.5 min
Radar cross-section—
Latest Orbital Elements
Epoch (UTC)2026-11-09 12:41:26
Mean motion14.91846743 rev/day
Eccentricity0.0005331
Inclination97.7197°
Right ascension of node208.0374°
Argument of perigee41.2357°
Mean anomaly318.9264°
B* drag term3.8881e-4
Element set999
Revolutions at epoch2,836
Mean elements (OMM) for the SGP4 model, refreshed every 6 hours. They describe the orbit at the epoch shown and drift as time passes, fastest for low orbits.
Source: CelesTrak satellite catalogue and GP data (celestrak.org); owner and manufacturer from GCAT (J. McDowell, CC BY 4.0).