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ICEYE-X60, 66753

Orbit data source: Space-Track

ICEYE-X60, 66753 is a Greek 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
66753, 2025-276CR
Orbit
SSO
Country
Flag of GRGR / GREC
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 (6 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: 1 day ago

TLE from 1 day ago
0 ICEYE-X60
1 66753U 25276CR  26144.21235416  .00003388  00000-0  21017-3 0  9996
2 66753  97.4178 217.6119 0004993 112.1572 248.0188 15.10366735 26743
Epoch: 2026-05-24T05:05Z
TLE epoch observation values (Epoch: 2026-05-24T05:05:47.399Z)
Latitude
-0.00004°
Longitude
-100.65333°
Altitude
539.451 km
Speed
7.592 km/s
True Right ascension
14h 30m 26s
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
13:55:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
535.51 km
Perigee altitude
528.61 km
Semi-major axis
6,910.197 km
Eccentricity
0.0005
Inclination
97.4178°
RAAN
217.6119°
Arg. of periapsis
112.1572°
True anomaly
247.96576°
Mean anomaly
248.0188°
Eccentric anomaly
247.99228°
Mean motion
3.7784 °/min
Orbital period
95.28 mins
BSTAR
0.00021017
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