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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Edit Public Description
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, 0.6 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 25287.94303745 .00002791 00000-0 26760-3 0 9997
2 63255 97.7108 179.3444 0001512 7.6427 352.4815 14.93919859 32014Epoch: 2025-10-14T22:37Z
TLE epoch observation values (Epoch: 2025-10-14T22:37:58.435Z)
Latitude
-0.00012°
Longitude
176.12672°
Altitude
587.729 km
Speed
7.567 km/s
True Right ascension
11h 57m 22s
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
05:49:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
583.794 km
Perigee altitude
581.689 km
Semi-major axis
6,960.878 km
Eccentricity
0.00015
Inclination
97.7108°
RAAN
179.3444°
Arg. of periapsis
7.6427°
True anomaly
352.47923°
Mean anomaly
352.4815°
Eccentric anomaly
352.48037°
Mean motion
3.73721 °/min
Orbital period
96.33 mins
BSTAR
0.0002676
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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 | 2025-10-15 16:26:36.932Z | 141.432° SSE | 2025-10-15 16:29:36.932Z | 91.255° ESE | 33.1° | 2025-10-15 16:33:36.932Z | 3.581° NNE |
| 6 mins | 2025-10-16 05:45:36.932Z | 13.596° NNE | 2025-10-16 05:47:36.932Z | 21.901° NNE | 44.208° | 2025-10-16 05:51:36.932Z | 192.584° SSW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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