Satellites/ICEYE-X84
ICEYE-X84
Satellite · FinlandActive
Who
Owner / operatorFIN
Manufacturer—
CountryFinland
Catalogue owner codeFIN
Orbit
OrbitingEarth
Orbit classLEO
Perigee586 km
Apogee594 km
Inclination52.98°
Period96.5 min
Radar cross-section—
Latest Orbital Elements
Epoch (UTC)2026-11-09 12:38:10
Mean motion14.92516825 rev/day
Eccentricity0.0005608
Inclination52.9845°
Right ascension of node234.5707°
Argument of perigee324.8587°
Mean anomaly35.2024°
B* drag term4.3540e-4
Element set999
Revolutions at epoch300
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).