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: 13 hours ago
TLE from 13 hours ago
0 ICEYE-X51
1 63257U 25052AZ 26083.52183491 .00004474 00000-0 35594-3 0 9997
2 63257 97.7375 338.8973 0002096 64.0955 296.0484 15.00918655 56105Epoch: 2026-03-24T12:31Z
TLE epoch observation values (Epoch: 2026-03-24T12:31:26.536Z)
Latitude
-0.00007°
Longitude
-30.96154°
Altitude
566.478 km
Speed
7.578 km/s
True Right ascension
22h 35m 35s
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
06:58:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.522 km
Perigee altitude
559.613 km
Semi-major axis
6,939.205 km
Eccentricity
0.00021
Inclination
97.7375°
RAAN
338.8973°
Arg. of periapsis
64.0955°
True anomaly
296.02682°
Mean anomaly
296.0484°
Eccentric anomaly
296.03761°
Mean motion
3.75473 °/min
Orbital period
95.88 mins
BSTAR
0.00035594
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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 | 2026-03-25 05:06:37.598Z | 48.754° ENE | 2026-03-25 05:08:37.598Z | 85.901° E | 22.666° | 2026-03-25 05:11:37.598Z | 145.389° SSE |
| 4 mins | 2026-03-25 06:42:37.598Z | 318.741° NNW | 2026-03-25 06:43:37.598Z | 297.519° NW | 21.214° | 2026-03-25 06:46:37.598Z | 242.735° WSW |
| 6 mins | 2026-03-25 17:27:37.598Z | 202.349° SSW | 2026-03-25 17:29:37.598Z | 249.777° W | 32.282° | 2026-03-25 17:33:37.598Z | 331.772° 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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