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ICEYE-X62, 66755

Orbit data source: Space-Track

ICEYE-X62, 66755 is a Polish 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.

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Identifier
66755, 2025-276CT
Orbit
SSO
Country
Flag of PLPL / POL
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 (4 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, 2.4 m
Radar Cross Section
0.776 m²

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago
0 ICEYE-X62
1 66755U 25276CT  26092.19347528  .00003704  00000-0  21768-3 0  9990
2 66755  97.4241 166.7578 0000700 235.6383 124.4781 15.12284956 18868
Epoch: 2026-04-02T04:38Z
TLE epoch observation values (Epoch: 2026-04-02T04:38:36.264Z)
Latitude
-0.00008°
Longitude
-93.43876°
Altitude
532.587 km
Speed
7.596 km/s
True Right ascension
11h 07m 01s
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
23:27:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
526.694 km
Perigee altitude
525.727 km
Semi-major axis
6,904.347 km
Eccentricity
0.00007
Inclination
97.4241°
RAAN
166.7578°
Arg. of periapsis
235.6383°
True anomaly
124.48471°
Mean anomaly
124.4781°
Eccentric anomaly
124.48141°
Mean motion
3.7832 °/min
Orbital period
95.16 mins
BSTAR
0.00021768
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