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, 0.8 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-X48
1 63253U 25052AV 26260.42438010 .00001939 00000-0 16716-3 0 9997
2 63253 97.6722 151.1637 0000866 252.4156 107.6972 14.98457304 82482Epoch: 2026-09-17T10:11Z
TLE epoch observation values (Epoch: 2026-09-17T10:11:06.440Z)
Latitude
-0.00004°
Longitude
2.02506°
Altitude
574.899 km
Speed
7.573 km/s
True Right ascension
10h 04m 39s
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
12:07:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
569.27 km
Perigee altitude
568.067 km
Semi-major axis
6,946.805 km
Eccentricity
0.00009
Inclination
97.6722°
RAAN
151.1637°
Arg. of periapsis
252.4156°
True anomaly
107.70665°
Mean anomaly
107.6972°
Eccentric anomaly
107.70193°
Mean motion
3.74857 °/min
Orbital period
96.04 mins
BSTAR
0.00016716
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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 | 2026-09-18 05:59:12.536Z | 359.205° N | 2026-09-18 06:02:12.536Z | 277.942° WNW | 55.834° | 2026-09-18 06:05:12.536Z | 210.719° SW |
| 6 mins | 2026-09-18 16:46:12.536Z | 160.659° S | 2026-09-18 16:49:12.536Z | 25.646° NE | 72.443° | 2026-09-18 16:52:12.536Z | 351.181° N |
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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