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: 6 hours ago
TLE from 6 hours ago
0 ICEYE-X52
1 64572U 25135AW 26046.31847380 .00003484 00000-0 34062-3 0 9999
2 64572 97.7605 162.0626 0002383 46.6458 313.4959 14.92993643 35699Epoch: 2026-02-15T07:38Z
TLE epoch observation values (Epoch: 2026-02-15T07:38:36.136Z)
Latitude
-0.00008°
Longitude
-97.91685°
Altitude
590.508 km
Speed
7.565 km/s
True Right ascension
10h 48m 15s
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
16:36:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.284 km
Perigee altitude
583.965 km
Semi-major axis
6,963.762 km
Eccentricity
0.00024
Inclination
97.7605°
RAAN
162.0626°
Arg. of periapsis
46.6458°
True anomaly
313.47609°
Mean anomaly
313.4959°
Eccentric anomaly
313.48599°
Mean motion
3.73489 °/min
Orbital period
96.39 mins
BSTAR
0.00034062
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-02-15 19:29:32.003Z | 54.208° ENE | 2026-02-15 19:31:32.003Z | 84.48° E | 16.351° | 2026-02-15 19:34:32.003Z | 132.877° SE |
| 5 mins | 2026-02-15 21:05:32.003Z | 339.189° N | 2026-02-15 21:07:32.003Z | 290.677° WNW | 29.98° | 2026-02-15 21:10:32.003Z | 228.41° WSW |
| 6 mins | 2026-02-16 07:54:32.003Z | 187.541° SSW | 2026-02-16 07:56:32.003Z | 236.192° WSW | 39.622° | 2026-02-16 08:00:32.003Z | 338.215° 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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