ICEYE-X50, 63255
Orbit data source: Space-Track
ICEYE-X50, 63255 is a payload satellite owned by ICEYE (FI) 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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63255 intel report (Beta)
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Identifier
Orbit
Country
FI / FINRelated 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, 2.4 m
Radar Cross Section
0.776 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 ICEYE-X50
1 63255U 25052AX 26083.49761757 .00002133 00000-0 20039-3 0 9996
2 63255 97.6980 336.9949 0003076 113.6864 246.4679 14.94971947 55991Epoch: 2026-03-24T11:56Z
TLE epoch observation values (Epoch: 2026-03-24T11:56:34.158Z)
Latitude
-0.00007°
Longitude
-24.12183°
Altitude
586.363 km
Speed
7.567 km/s
True Right ascension
22h 27m 58s
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
08:45:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
581.612 km
Perigee altitude
577.332 km
Semi-major axis
6,957.609 km
Eccentricity
0.00031
Inclination
97.698°
RAAN
336.9949°
Arg. of periapsis
113.6864°
True anomaly
246.43559°
Mean anomaly
246.4679°
Eccentric anomaly
246.45174°
Mean motion
3.73984 °/min
Orbital period
96.26 mins
BSTAR
0.00020039
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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-X50 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 04:36:19.800Z | 63.346° ENE | 2026-03-25 04:38:19.800Z | 94.343° ESE | 13.909° | 2026-03-25 04:40:19.800Z | 124.317° SE |
| 6 mins | 2026-03-25 06:11:19.800Z | 347.994° N | 2026-03-25 06:13:19.800Z | 304.698° NW | 32.867° | 2026-03-25 06:17:19.800Z | 218.161° SW |
| 6 mins | 2026-03-25 16:59:19.800Z | 175.412° S | 2026-03-25 17:02:19.800Z | 284.651° WNW | 43.496° | 2026-03-25 17:05:19.800Z | 342.159° N |
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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