ICEYE-X52, 64572
Orbit data source: Space-Track
ICEYE-X52, 64572 is a payload satellite owned by ICEYE (FI) in SSO that was launched on Mon, 23 Jun 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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64572 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, 0.8 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-X52
1 64572U 25135AW 25328.19578053 .00003446 00000-0 34207-3 0 9994
2 64572 97.7609 80.0998 0000768 323.1895 36.9271 14.92388256 23292Epoch: 2025-11-24T04:41Z
TLE epoch observation values (Epoch: 2025-11-24T04:41:55.437Z)
Latitude
-0.00007°
Longitude
-53.78041°
Altitude
593.106 km
Speed
7.564 km/s
True Right ascension
05h 20m 23s
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
10:44:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
588.044 km
Perigee altitude
586.974 km
Semi-major axis
6,965.646 km
Eccentricity
0.00008
Inclination
97.7609°
RAAN
80.0998°
Arg. of periapsis
323.1895°
True anomaly
36.93239°
Mean anomaly
36.9271°
Eccentric anomaly
36.92974°
Mean motion
3.73337 °/min
Orbital period
96.43 mins
BSTAR
0.00034207
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Other satellites on launch #135 in the year 2025 (2025-06-23 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-X52 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 | 2025-11-24 19:45:28.179Z | 40.424° NE | 2025-11-24 19:48:28.179Z | 90.98° ESE | 23.952° | 2025-11-24 19:51:28.179Z | 147.732° SSE |
| 4 mins | 2025-11-24 21:22:28.179Z | 323.972° NNW | 2025-11-24 21:24:28.179Z | 282.086° WNW | 21.517° | 2025-11-24 21:26:28.179Z | 247.223° WSW |
| 6 mins | 2025-11-25 08:11:28.179Z | 207.54° SW | 2025-11-25 08:13:28.179Z | 252.661° W | 30.295° | 2025-11-25 08:17:28.179Z | 329.285° 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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