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: 13 hours ago
TLE from 13 hours ago
0 ICEYE-X50
1 63255U 25052AX 26260.49766024 .00001355 00000-0 12737-3 0 9996
2 63255 97.6739 150.5643 0000353 241.4877 118.6308 14.95521958 82446Epoch: 2026-09-17T11:56Z
TLE epoch observation values (Epoch: 2026-09-17T11:56:37.844Z)
Latitude
-0.00009°
Longitude
-25.02742°
Altitude
583.92 km
Speed
7.568 km/s
True Right ascension
10h 02m 15s
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
17:17:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
578.009 km
Perigee altitude
577.518 km
Semi-major axis
6,955.9 km
Eccentricity
0.00004
Inclination
97.6739°
RAAN
150.5643°
Arg. of periapsis
241.4877°
True anomaly
118.63435°
Mean anomaly
118.6308°
Eccentric anomaly
118.63258°
Mean motion
3.74122 °/min
Orbital period
96.23 mins
BSTAR
0.00012737
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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 | 2026-09-18 04:36:03.714Z | 62.734° ENE | 2026-09-18 04:38:03.714Z | 95.095° ESE | 15.808° | 2026-09-18 04:40:03.714Z | 126.228° SE |
| 6 mins | 2026-09-18 06:11:03.714Z | 344.67° N | 2026-09-18 06:13:03.714Z | 300.364° NW | 37.56° | 2026-09-18 06:17:03.714Z | 220.457° SW |
| 7 mins | 2026-09-18 16:58:03.714Z | 176.642° S | 2026-09-18 17:01:03.714Z | 217.66° SW | 61.486° | 2026-09-18 17:05:03.714Z | 341.201° 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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