ICEYE-X51, 63257
Orbit data source: Space-Track
ICEYE-X51, 63257 is a payload satellite owned by ICEYE US (US) in SSO that was launched on Sat, 15 Mar 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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63257 intel report (Beta)
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Identifier
Orbit
Country
USRelated 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, 0.7 m
Radar Cross Section
0.776 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 ICEYE-X51
1 63257U 25052AZ 26129.85654353 .00003197 00000-0 25597-3 0 9997
2 63257 97.7471 25.0534 0002013 63.7760 296.3671 15.00888736 63058Epoch: 2026-05-09T20:33Z
TLE epoch observation values (Epoch: 2026-05-09T20:33:25.360Z)
Latitude
-0.00001°
Longitude
-150.97024°
Altitude
566.588 km
Speed
7.578 km/s
True Right ascension
01h 40m 12s
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
15:07:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.558 km
Perigee altitude
559.764 km
Semi-major axis
6,939.298 km
Eccentricity
0.0002
Inclination
97.7471°
RAAN
25.0534°
Arg. of periapsis
63.776°
True anomaly
296.34643°
Mean anomaly
296.3671°
Eccentric anomaly
296.35677°
Mean motion
3.75465 °/min
Orbital period
95.88 mins
BSTAR
0.00025597
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Other satellites on launch #52 in the year 2025 (2025-03-15 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-X51 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 | 2026-05-10 15:55:00.301Z | 101.096° ESE | 2026-05-10 15:57:00.301Z | 70.577° E | 14.679° | 2026-05-10 15:59:00.301Z | 37.596° NE |
| 5 mins | 2026-05-10 17:30:00.301Z | 207.29° SW | 2026-05-10 17:32:00.301Z | 265.01° W | 32.546° | 2026-05-10 17:35:00.301Z | 327.772° NNW |
| 5 mins | 2026-05-11 05:09:00.301Z | 53.425° ENE | 2026-05-11 05:11:00.301Z | 94.733° ESE | 23.004° | 2026-05-11 05:14:00.301Z | 149.095° SSE |
| 5 mins | 2026-05-11 06:44:00.301Z | 329.435° NNW | 2026-05-11 06:46:00.301Z | 289.283° WNW | 21.346° | 2026-05-11 06:49:00.301Z | 239.316° WSW |
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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