Satellites/ICEYE-X80
ICEYE-X80
Satellite · FinlandActive
Who
Owner / operatorICEYE
ManufacturerICEYE
CountryFinland
Catalogue owner codeFIN
Orbit
OrbitingEarth
Orbit classLEO
Perigee588 km
Apogee597 km
Inclination97.74°
Period96.5 min
Radar cross-section—
Latest Orbital Elements
Epoch (UTC)2026-11-09 07:43:23
Mean motion14.91756258 rev/day
Eccentricity0.0006874
Inclination97.7435°
Right ascension of node211.6105°
Argument of perigee87.687°
Mean anomaly272.5136°
B* drag term4.1597e-4
Element set999
Revolutions at epoch1,863
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).