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.
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55049 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
FI / FINRelated business
Manufacturer
ICEYE
Mission
Operational Commercial Radar Imaging
Bus & Motor
ICEYE, Unknown motor
Mass
80 kg wet, 80 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
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 & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 ICEYE-X21
1 55049U 23001AS 25286.96697354 .00052273 00000-0 92014-3 0 9999
2 55049 97.3611 355.1999 0014459 233.4933 126.4987 15.50177106154913Epoch: 2025-10-13T23:12Z
TLE epoch observation values (Epoch: 2025-10-13T23:12:26.513Z)
Latitude
-0.00009°
Longitude
-15.67272°
Altitude
425.195 km
Speed
7.653 km/s
True Right ascension
23h 40m 47s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
02:52:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
422.952 km
Perigee altitude
403.313 km
Semi-major axis
6,791.269 km
Eccentricity
0.00145
Inclination
97.3611°
RAAN
355.1999°
Arg. of periapsis
233.4933°
True anomaly
126.63175°
Mean anomaly
126.4987°
Eccentric anomaly
126.56524°
Mean motion
3.87808 °/min
Orbital period
92.83 mins
BSTAR
0.00092014
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Other satellites on launch #1 in the year 2023 (2023-01-03 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ICEYE-X21 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-14 16:49:09.406Z | 49.134° ENE | 2025-10-14 16:51:09.406Z | 90.141° ESE | 18.199° | 2025-10-14 16:53:09.406Z | 136.029° SSE |
| 4 mins | 2025-10-15 04:47:09.406Z | 173.083° S | 2025-10-15 04:49:09.406Z | 320.483° NNW | 43.197° | 2025-10-15 04:51:09.406Z | 344.65° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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