Showing default

ICEYE-X59, 66752

Orbit data source: Space-Track

ICEYE-X59, 66752 is a Finnish payload satellite in SSO that was launched on Fri, 28 Nov 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

Loading next visibility...
Identifier
66752, 2025-276CQ
Orbit
SSO
Country
Flag of FIFI / FIN
Related business
Manufacturer
ICEYE
Mission
Operational Commercial Radar Imaging
Bus & Motor
ICEYE, Unknown motor
Mass
120 kg wet, 120 kg dry
Launch date (UTC)
2025-11-28 (2 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 1 Pan, 0.8 m
Radar Cross Section
0.776 m²

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 ICEYE-X59
1 66752U 25276CQ  26034.17244480  .00003521  00000-0  18577-3 0  9995
2 66752  97.4342 109.9796 0004589 102.4668 257.7079 15.16182461 10071
Epoch: 2026-02-03T04:08Z
TLE epoch observation values (Epoch: 2026-02-03T04:08:19.230Z)
Latitude
-0°
Longitude
-85.45772°
Altitude
521.151 km
Speed
7.602 km/s
True Right ascension
07h 19m 55s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
07:05:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
517.526 km
Perigee altitude
511.2 km
Semi-major axis
6,892.5 km
Eccentricity
0.00046
Inclination
97.4342°
RAAN
109.9796°
Arg. of periapsis
102.4668°
True anomaly
257.65653°
Mean anomaly
257.7079°
Eccentric anomaly
257.68221°
Mean motion
3.79296 °/min
Orbital period
94.91 mins
BSTAR
0.00018577
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|