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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Edit Public Description
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 25334.65192272 .00004896 00000-0 46540-3 0 9993
2 63253 97.7073 224.9268 0003134 120.0903 240.0628 14.93917706 38979Epoch: 2025-11-30T15:38Z
TLE epoch observation values (Epoch: 2025-11-30T15:38:46.123Z)
Latitude
-0.00001°
Longitude
-79.52809°
Altitude
589.87 km
Speed
7.565 km/s
True Right ascension
14h 59m 42s
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
23:16:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
584.929 km
Perigee altitude
580.566 km
Semi-major axis
6,960.885 km
Eccentricity
0.00031
Inclination
97.7073°
RAAN
224.9268°
Arg. of periapsis
120.0903°
True anomaly
240.03168°
Mean anomaly
240.0628°
Eccentric anomaly
240.04724°
Mean motion
3.7372 °/min
Orbital period
96.33 mins
BSTAR
0.0004654
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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 | 2025-12-01 05:05:08.249Z | 39.775° NE | 2025-12-01 05:08:08.249Z | 98.309° ESE | 26.782° | 2025-12-01 05:11:08.249Z | 154.737° SSE |
| 4 mins | 2025-12-01 06:42:08.249Z | 315.447° NNW | 2025-12-01 06:43:08.249Z | 295.982° NW | 19.177° | 2025-12-01 06:46:08.249Z | 246.371° WSW |
| 4 mins | 2025-12-01 15:56:08.249Z | 88.253° E | 2025-12-01 15:57:08.249Z | 68.959° E | 18.593° | 2025-12-01 16:00:08.249Z | 21.509° NNE |
| 5 mins | 2025-12-01 17:30:08.249Z | 211.935° SW | 2025-12-01 17:32:08.249Z | 254.386° W | 27.549° | 2025-12-01 17:35:08.249Z | 318.903° 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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