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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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, 2.4 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-X52
1 64572U 25135AW 26289.91886725 .00001875 00000-0 18142-3 0 9993
2 64572 97.7852 42.9304 0000541 303.0752 57.0415 14.93964465 72053Epoch: 2026-10-16T22:03Z
TLE epoch observation values (Epoch: 2026-10-16T22:03:10.130Z)
Latitude
-0.00011°
Longitude
46.70523°
Altitude
588.428 km
Speed
7.566 km/s
True Right ascension
02h 51m 43s
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
03:11:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
582.982 km
Perigee altitude
582.229 km
Semi-major axis
6,960.743 km
Eccentricity
0.00005
Inclination
97.7852°
RAAN
42.9304°
Arg. of periapsis
303.0752°
True anomaly
57.0467°
Mean anomaly
57.0415°
Eccentric anomaly
57.0441°
Mean motion
3.73732 °/min
Orbital period
96.33 mins
BSTAR
0.00018142
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-10-17 19:32:38.983Z | 57.829° ENE | 2026-10-17 19:34:38.983Z | 89.77° E | 17.243° | 2026-10-17 19:36:38.983Z | 123.678° SE |
| 6 mins | 2026-10-17 21:07:38.983Z | 346.731° N | 2026-10-17 21:10:38.983Z | 278.776° WNW | 35.15° | 2026-10-17 21:13:38.983Z | 225.479° WSW |
| 6 mins | 2026-10-18 07:56:38.983Z | 185.326° SSW | 2026-10-18 07:59:38.983Z | 292.526° NW | 54.874° | 2026-10-18 08:02:38.983Z | 338.032° N |
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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