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: 16 hours ago
TLE from 16 hours ago
0 ICEYE-X52
1 64572U 25135AW 26224.61061664 .00000894 00000-0 89763-4 0 9994
2 64572 97.7789 338.2577 0003171 122.3141 237.8386 14.93737343 62306Epoch: 2026-08-12T14:39Z
TLE epoch observation values (Epoch: 2026-08-12T14:39:17.277Z)
Latitude
-0.00006°
Longitude
157.37365°
Altitude
590.515 km
Speed
7.564 km/s
True Right ascension
22h 33m 01s
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
21:01:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
585.519 km
Perigee altitude
581.104 km
Semi-major axis
6,961.449 km
Eccentricity
0.00032
Inclination
97.7789°
RAAN
338.2577°
Arg. of periapsis
122.3141°
True anomaly
237.80785°
Mean anomaly
237.8386°
Eccentric anomaly
237.82322°
Mean motion
3.73675 °/min
Orbital period
96.34 mins
BSTAR
0.000089763
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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 | 2026-08-13 06:52:38.885Z | 118.914° SE | 2026-08-13 06:55:38.885Z | 63.274° ENE | 22.876° | 2026-08-13 06:58:38.885Z | 15.035° NNE |
| 5 mins | 2026-08-13 08:28:38.885Z | 222.829° SW | 2026-08-13 08:30:38.885Z | 261.853° W | 22.428° | 2026-08-13 08:33:38.885Z | 315.378° NNW |
| 6 mins | 2026-08-13 20:10:38.885Z | 32.64° NE | 2026-08-13 20:13:38.885Z | 121.311° SE | 35.525° | 2026-08-13 20:16:38.885Z | 172.27° S |
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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