Satellites/ICEYE-X81
ICEYE-X81
Satellite · FinlandActive
Who
Owner / operatorICEYE
ManufacturerICEYE
CountryFinland
Catalogue owner codeUS
Orbit
OrbitingEarth
Orbit classLEO
Perigee584 km
Apogee593 km
Inclination97.74°
Period96.5 min
Radar cross-section—
Latest Orbital Elements
Epoch (UTC)2026-11-09 04:00:01
Mean motion14.93076077 rev/day
Eccentricity0.0006595
Inclination97.7443°
Right ascension of node211.5024°
Argument of perigee90.3926°
Mean anomaly236.02°
B* drag term6.4096e-3
Element set999
Revolutions at epoch564
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).