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: 17 hours ago
TLE from 17 hours ago
0 ICEYE-X51
1 63257U 25052AZ 26083.92183853 .00004306 00000-0 34275-3 0 9992
2 63257 97.7376 339.2957 0002135 61.9846 298.1594 15.00922640 56162Epoch: 2026-03-24T22:07Z
TLE epoch observation values (Epoch: 2026-03-24T22:07:26.848Z)
Latitude
-0.00001°
Longitude
-174.95872°
Altitude
566.405 km
Speed
7.578 km/s
True Right ascension
22h 37m 10s
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
20:32:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.537 km
Perigee altitude
559.574 km
Semi-major axis
6,939.193 km
Eccentricity
0.00021
Inclination
97.7376°
RAAN
339.2957°
Arg. of periapsis
61.9846°
True anomaly
298.13783°
Mean anomaly
298.1594°
Eccentric anomaly
298.14861°
Mean motion
3.75474 °/min
Orbital period
95.88 mins
BSTAR
0.00034275
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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 | 2026-03-25 15:53:07.819Z | 99.501° ESE | 2026-03-25 15:55:07.819Z | 68.323° E | 14.692° | 2026-03-25 15:57:07.819Z | 35.905° NE |
| 5 mins | 2026-03-25 17:28:07.819Z | 209.154° SW | 2026-03-25 17:30:07.819Z | 270.269° WNW | 32.433° | 2026-03-25 17:33:07.819Z | 328.76° NNW |
| 5 mins | 2026-03-26 05:07:07.819Z | 55.6° ENE | 2026-03-26 05:09:07.819Z | 98.433° ESE | 22.958° | 2026-03-26 05:12:07.819Z | 150.429° SSE |
| 4 mins | 2026-03-26 06:42:07.819Z | 327.235° NNW | 2026-03-26 06:44:07.819Z | 285.795° WNW | 21.281° | 2026-03-26 06:46:07.819Z | 248.547° W |
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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