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: 7 hours ago
TLE from 7 hours ago
0 ICEYE-X21
1 55049U 23001AS 25336.17515589 .00074116 00000-0 10099-2 0 9999
2 55049 97.3573 45.6985 0011222 52.2630 307.9640 15.57215269162553Epoch: 2025-12-02T04:12Z
TLE epoch observation values (Epoch: 2025-12-02T04:12:13.468Z)
Latitude
-0.00011°
Longitude
-88.62168°
Altitude
394.191 km
Speed
7.676 km/s
True Right ascension
03h 02m 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
09:17:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
400.233 km
Perigee altitude
385.037 km
Semi-major axis
6,770.772 km
Eccentricity
0.00112
Inclination
97.3573°
RAAN
45.6985°
Arg. of periapsis
52.263°
True anomaly
307.86253°
Mean anomaly
307.964°
Eccentric anomaly
307.91327°
Mean motion
3.8957 °/min
Orbital period
92.41 mins
BSTAR
0.0010099
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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 | 2025-12-02 17:06:34.047Z | 46.297° ENE | 2025-12-02 17:08:34.047Z | 96.675° ESE | 22.474° | 2025-12-02 17:10:34.047Z | 147.335° SSE |
| 4 mins | 2025-12-03 05:01:34.047Z | 187.232° SSW | 2025-12-03 05:02:34.047Z | 221.498° SW | 39.576° | 2025-12-03 05:05:34.047Z | 340.125° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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