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ICEYE-X58, 66751

Orbit data source: Space-Track

ICEYE-X58, 66751 is a payload satellite owned by ICEYE (FI) 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.

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Identifier
66751, 2025-276CP
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: 5 hours ago

TLE from 5 hours ago
0 ICEYE-X58
1 66751U 25276CP  26035.19462880  .00004304  00000-0  21327-3 0  9990
2 66751  97.4343 111.0622 0004733  84.1262 276.0511 15.18275560 10238
Epoch: 2026-02-04T04:40Z
TLE epoch observation values (Epoch: 2026-02-04T04:40:15.928Z)
Latitude
-0.00007°
Longitude
-93.36886°
Altitude
513.797 km
Speed
7.607 km/s
True Right ascension
07h 24m 14s
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
11:54:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
511.281 km
Perigee altitude
504.762 km
Semi-major axis
6,886.158 km
Eccentricity
0.00047
Inclination
97.4343°
RAAN
111.0622°
Arg. of periapsis
84.1262°
True anomaly
275.99716°
Mean anomaly
276.0511°
Eccentric anomaly
276.02413°
Mean motion
3.7982 °/min
Orbital period
94.78 mins
BSTAR
0.00021327
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