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ICEYE-X62, 66755

Orbit data source: Space-Track

ICEYE-X62, 66755 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
66755, 2025-276CT
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-X62
1 66755U 25276CT  26034.21398366  .00004624  00000-0  23001-3 0  9999
2 66755  97.4343 110.0716 0003711 103.5119 256.6529 15.18105987 10088
Epoch: 2026-02-03T05:08Z
TLE epoch observation values (Epoch: 2026-02-03T05:08:08.188Z)
Latitude
0.00002°
Longitude
-100.36065°
Altitude
515.243 km
Speed
7.606 km/s
True Right ascension
07h 20m 17s
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
07:05:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
511.09 km
Perigee altitude
505.979 km
Semi-major axis
6,886.672 km
Eccentricity
0.00037
Inclination
97.4343°
RAAN
110.0716°
Arg. of periapsis
103.5119°
True anomaly
256.61153°
Mean anomaly
256.6529°
Eccentric anomaly
256.63221°
Mean motion
3.79777 °/min
Orbital period
94.79 mins
BSTAR
0.00023001
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