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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Edit Public Description
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: 12 hours ago
TLE from 12 hours ago
0 ICEYE-X51
1 63257U 25052AZ 25287.97510169 .00006232 00000-0 55237-3 0 9997
2 63257 97.7080 179.5520 0001953 71.2556 288.8877 14.96571696 32039Epoch: 2025-10-14T23:24Z
TLE epoch observation values (Epoch: 2025-10-14T23:24:08.786Z)
Latitude
-0.00009°
Longitude
164.75959°
Altitude
580.109 km
Speed
7.571 km/s
True Right ascension
11h 58m 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
05:48:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
575.867 km
Perigee altitude
573.151 km
Semi-major axis
6,952.646 km
Eccentricity
0.0002
Inclination
97.708°
RAAN
179.552°
Arg. of periapsis
71.2556°
True anomaly
288.86652°
Mean anomaly
288.8877°
Eccentric anomaly
288.87711°
Mean motion
3.74385 °/min
Orbital period
96.16 mins
BSTAR
0.00055237
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-15 17:11:01.713Z | 185.255° SSW | 2025-10-15 17:14:01.713Z | 274.772° WNW | 39.622° | 2025-10-15 17:17:01.713Z | 336.243° NNW |
| 4 mins | 2025-10-16 04:53:01.713Z | 59.861° ENE | 2025-10-16 04:55:01.713Z | 97.028° ESE | 18.993° | 2025-10-16 04:57:01.713Z | 132.412° SE |
| 5 mins | 2025-10-16 06:28:01.713Z | 336.507° NNW | 2025-10-16 06:30:01.713Z | 293.657° NW | 26.113° | 2025-10-16 06:33:01.713Z | 234.472° 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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