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, 0.8 m
Radar Cross Section
0.776 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 ICEYE-X51
1 63257U 25052AZ 26260.26132485 .00003198 00000-0 25623-3 0 9996
2 63257 97.7703 155.2603 0001843 59.9251 300.2155 15.00865298 82614Epoch: 2026-09-17T06:16Z
TLE epoch observation values (Epoch: 2026-09-17T06:16:18.467Z)
Latitude
-0.00002°
Longitude
64.98226°
Altitude
566.637 km
Speed
7.578 km/s
True Right ascension
10h 21m 02s
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
05:13:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.513 km
Perigee altitude
559.955 km
Semi-major axis
6,939.371 km
Eccentricity
0.00018
Inclination
97.7703°
RAAN
155.2603°
Arg. of periapsis
59.9251°
True anomaly
300.19725°
Mean anomaly
300.2155°
Eccentric anomaly
300.20637°
Mean motion
3.75459 °/min
Orbital period
95.88 mins
BSTAR
0.00025623
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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 | 2026-09-17 17:36:36.831Z | 204.176° SW | 2026-09-17 17:38:36.831Z | 255.025° W | 39.521° | 2026-09-17 17:41:36.831Z | 325.69° NNW |
| 5 mins | 2026-09-18 05:15:36.831Z | 49.272° ENE | 2026-09-18 05:17:36.831Z | 87.056° E | 25.108° | 2026-09-18 05:20:36.831Z | 146.09° SSE |
| 4 mins | 2026-09-18 06:51:36.831Z | 317.756° NNW | 2026-09-18 06:52:36.831Z | 296.41° NW | 22.968° | 2026-09-18 06:55:36.831Z | 242.458° 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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