ICEYE-X48, 63253
Orbit data source: Space-Track
ICEYE-X48, 63253 is a payload satellite owned by ICEYE US (US) 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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63253 intel report (Beta)
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Identifier
Orbit
Country
USRelated 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, 0.7 m
Radar Cross Section
0.776 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 ICEYE-X48
1 63253U 25052AV 26175.20369027 .00001670 00000-0 14641-3 0 9996
2 63253 97.6882 67.2848 0002403 134.4621 225.6798 14.97999448 69723Epoch: 2026-06-24T04:53Z
TLE epoch observation values (Epoch: 2026-06-24T04:53:18.839Z)
Latitude
-0.00003°
Longitude
81.59204°
Altitude
577.298 km
Speed
7.571 km/s
True Right ascension
04h 29m 08s
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
02:13:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
571.755 km
Perigee altitude
568.416 km
Semi-major axis
6,948.223 km
Eccentricity
0.00024
Inclination
97.6882°
RAAN
67.2848°
Arg. of periapsis
134.4621°
True anomaly
225.6601°
Mean anomaly
225.6798°
Eccentric anomaly
225.66995°
Mean motion
3.74742 °/min
Orbital period
96.07 mins
BSTAR
0.00014641
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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-X48 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-24 16:14:37.481Z | 132.417° SE | 2026-06-24 16:17:37.481Z | 79.612° E | 28.047° | 2026-06-24 16:20:37.481Z | 14.557° NNE |
| 4 mins | 2026-06-24 17:51:37.481Z | 239.183° WSW | 2026-06-24 17:53:37.481Z | 275.829° WNW | 16.883° | 2026-06-24 17:55:37.481Z | 306.938° NW |
| 6 mins | 2026-06-25 05:30:37.481Z | 22.427° NNE | 2026-06-25 05:33:37.481Z | 108.733° ESE | 41.675° | 2026-06-25 05:36:37.481Z | 180.055° SSW |
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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