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: 9 hours ago
TLE from 9 hours ago
0 ICEYE-X50
1 63255U 25052AX 26265.58264042 .00001474 00000-0 13813-3 0 9992
2 63255 97.6736 155.5444 0000663 177.4446 182.6778 14.95534881 83207Epoch: 2026-09-22T13:59Z
TLE epoch observation values (Epoch: 2026-09-22T13:59:00.132Z)
Latitude
-0.00007°
Longitude
-55.65218°
Altitude
584.223 km
Speed
7.568 km/s
True Right ascension
10h 22m 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
15:36:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
578.184 km
Perigee altitude
577.262 km
Semi-major axis
6,955.86 km
Eccentricity
0.00007
Inclination
97.6736°
RAAN
155.5444°
Arg. of periapsis
177.4446°
True anomaly
182.67745°
Mean anomaly
182.6778°
Eccentric anomaly
182.67762°
Mean motion
3.74125 °/min
Orbital period
96.22 mins
BSTAR
0.00013813
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-09-23 05:00:24.224Z | 35.636° NE | 2026-09-23 05:03:24.224Z | 84.529° E | 29.829° | 2026-09-23 05:07:24.224Z | 158.993° S |
| 4 mins | 2026-09-23 06:37:24.224Z | 321.591° NNW | 2026-09-23 06:39:24.224Z | 283.026° WNW | 20.044° | 2026-09-23 06:41:24.224Z | 250.521° W |
| 4 mins | 2026-09-23 15:50:24.224Z | 99.583° ESE | 2026-09-23 15:52:24.224Z | 63.559° ENE | 19.196° | 2026-09-23 15:54:24.224Z | 30.076° NE |
| 5 mins | 2026-09-23 17:25:24.224Z | 216.284° SW | 2026-09-23 17:27:24.224Z | 265.801° W | 32.584° | 2026-09-23 17:30:24.224Z | 323.018° NNW |
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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