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ICEYE-X21, 55049

Orbit data source: Space-Track

ICEYE-X21, 55049 is a payload satellite owned by ICEYE (FI) in SSO 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
55049, 2023-001AS
Orbit
SSO
Country
Flag of FIFI / FIN
Related business
Manufacturer
ICEYE
Mission
Operational Commercial Radar Imaging
Bus & Motor
ICEYE, Unknown motor
Mass
80 kg wet, 80 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, 2.4 m
Radar Cross Section
1.837 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 6 hours ago

TLE from 6 hours ago
0 ICEYE-X21
1 55049U 23001AS  26166.47555300  .00420513  89657-4  46993-3 0  9997
2 55049  97.3049 252.8743 0003678 243.9240 116.1665 16.09455492193347
Epoch: 2026-06-15T11:24Z
TLE epoch observation values (Epoch: 2026-06-15T11:24:47.779Z)
Latitude
-0.00002°
Longitude
177.91382°
Altitude
252.627 km
Speed
7.755 km/s
True Right ascension
16h 51m 29s
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
03:54:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
247.617 km
Perigee altitude
242.745 km
Semi-major axis
6,623.318 km
Eccentricity
0.00037
Inclination
97.3049°
RAAN
252.8743°
Arg. of periapsis
243.924°
True anomaly
116.20432°
Mean anomaly
116.1665°
Eccentric anomaly
116.18541°
Mean motion
4.02652 °/min
Orbital period
89.41 mins
BSTAR
0.00046993
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