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ICEYE-X27, 55062

Orbit data source: Space-Track

ICEYE-X27, 55062 is a payload satellite owned by ICEYE US (US) in LEO that was launched on Tue, 03 Jan 2023 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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.

Not visible in the next 10 days
Identifier
55062, 2023-001BF
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
ICEYE
Mission
Non-operational Commercial Radar Imaging
Bus & Motor
ICEYE, Unknown motor
Mass
90 kg wet, 89 kg dry
Launch date (UTC)
2023-01-03 (3 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 1 Pan, 1.6 m
Radar Cross Section
1.837 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 3 weeks ago

TLE from 3 weeks ago
0 ICEYE-X27
1 55062U 23001BF  25318.86992713  .04692071  24341-5  12755-2 0  9998
2 55062  97.3286  33.5720 0006493 268.5925  91.4624 16.28134525160240
Epoch: 2025-11-14T20:52Z
TLE epoch observation values (Epoch: 2025-11-14T20:52:41.704Z)
Latitude
-0.00005°
Longitude
26.19101°
Altitude
200.907 km
Speed
7.786 km/s
True Right ascension
02h 14m 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
08:19:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
198.645 km
Perigee altitude
190.11 km
Semi-major axis
6,572.515 km
Eccentricity
0.00065
Inclination
97.3286°
RAAN
33.572°
Arg. of periapsis
268.5925°
True anomaly
91.53678°
Mean anomaly
91.4624°
Eccentric anomaly
91.49959°
Mean motion
4.07329 °/min
Orbital period
88.38 mins
BSTAR
0.0012755
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Computing Atmospheric mass density...

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