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: 7 hours ago
TLE from 7 hours ago
0 ICEYE-X51
1 63257U 25052AZ 26220.59308337 .00002471 00000-0 19892-3 0 9993
2 63257 97.7648 115.6111 0001979 61.3294 298.8129 15.00882685 76660Epoch: 2026-08-08T14:14Z
TLE epoch observation values (Epoch: 2026-08-08T14:14:02.403Z)
Latitude
0.00005°
Longitude
-55.00112°
Altitude
566.565 km
Speed
7.578 km/s
True Right ascension
07h 42m 26s
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
11:38:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.553 km
Perigee altitude
559.807 km
Semi-major axis
6,939.317 km
Eccentricity
0.0002
Inclination
97.7648°
RAAN
115.6111°
Arg. of periapsis
61.3294°
True anomaly
298.79303°
Mean anomaly
298.8129°
Eccentric anomaly
298.80296°
Mean motion
3.75464 °/min
Orbital period
95.88 mins
BSTAR
0.00019892
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-08-09 05:13:05.734Z | 46.95° ENE | 2026-08-09 05:16:05.734Z | 107.242° ESE | 22.618° | 2026-08-09 05:18:05.734Z | 143.736° SSE |
| 4 mins | 2026-08-09 06:49:05.734Z | 321.449° NNW | 2026-08-09 06:50:05.734Z | 301.003° NW | 20.995° | 2026-08-09 06:53:05.734Z | 244.442° WSW |
| 6 mins | 2026-08-09 17:34:05.734Z | 200.781° SSW | 2026-08-09 17:36:05.734Z | 243.521° WSW | 31.614° | 2026-08-09 17:40:05.734Z | 330.647° NNW |
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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