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: 1 day ago
TLE from 1 day ago
0 ICEYE-X48
1 63253U 25052AV 26234.64684177 .00002928 00000-0 25107-3 0 9992
2 63253 97.6774 125.8003 0002468 41.0441 319.0967 14.98284540 78627Epoch: 2026-08-22T15:31Z
TLE epoch observation values (Epoch: 2026-08-22T15:31:27.128Z)
Latitude
-0.00004°
Longitude
-78.01698°
Altitude
573.953 km
Speed
7.575 km/s
True Right ascension
08h 23m 12s
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
13:59:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
570.918 km
Perigee altitude
567.488 km
Semi-major axis
6,947.34 km
Eccentricity
0.00025
Inclination
97.6774°
RAAN
125.8003°
Arg. of periapsis
41.0441°
True anomaly
319.07818°
Mean anomaly
319.0967°
Eccentric anomaly
319.08744°
Mean motion
3.74814 °/min
Orbital period
96.05 mins
BSTAR
0.00025107
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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 | 2026-08-24 04:58:11.360Z | 44.024° NE | 2026-08-24 05:01:11.360Z | 101.037° ESE | 23.391° | 2026-08-24 05:04:11.360Z | 151.554° SSE |
| 5 mins | 2026-08-24 06:34:11.360Z | 327.815° NNW | 2026-08-24 06:36:11.360Z | 287.335° WNW | 21.321° | 2026-08-24 06:39:11.360Z | 238.929° WSW |
| 5 mins | 2026-08-24 17:21:11.360Z | 207.841° SW | 2026-08-24 17:23:11.360Z | 262.523° W | 32.031° | 2026-08-24 17:26:11.360Z | 326.56° NNW |
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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