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: 8 hours ago
TLE from 8 hours ago
0 ICEYE-X50
1 63255U 25052AX 26175.25117230 .00001779 00000-0 16662-3 0 9995
2 63255 97.6889 67.0108 0002326 139.3156 220.8239 14.95300329 69707Epoch: 2026-06-24T06:01Z
TLE epoch observation values (Epoch: 2026-06-24T06:01:41.286Z)
Latitude
-0.00004°
Longitude
64.17771°
Altitude
585.715 km
Speed
7.567 km/s
True Right ascension
04h 28m 02s
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
00:46:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
580.07 km
Perigee altitude
576.834 km
Semi-major axis
6,956.589 km
Eccentricity
0.00023
Inclination
97.6889°
RAAN
67.0108°
Arg. of periapsis
139.3156°
True anomaly
220.80648°
Mean anomaly
220.8239°
Eccentric anomaly
220.81519°
Mean motion
3.74066 °/min
Orbital period
96.24 mins
BSTAR
0.00016662
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-24 15:49:21.208Z | 103.961° ESE | 2026-06-24 15:51:21.208Z | 71.674° E | 17.111° | 2026-06-24 15:54:21.208Z | 24.275° NE |
| 6 mins | 2026-06-24 17:24:21.208Z | 208.038° SW | 2026-06-24 17:26:21.208Z | 251.491° W | 29.323° | 2026-06-24 17:30:21.208Z | 328.556° NNW |
| 5 mins | 2026-06-25 05:06:21.208Z | 48.357° ENE | 2026-06-25 05:08:21.208Z | 95.217° ESE | 28.121° | 2026-06-25 05:11:21.208Z | 155.95° SSE |
| 4 mins | 2026-06-25 06:42:21.208Z | 314.921° NW | 2026-06-25 06:43:21.208Z | 296.146° NW | 18.066° | 2026-06-25 06:46:21.208Z | 247.925° 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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