ICEYE-X54, 64570
Orbit data source: Space-Track
ICEYE-X54, 64570 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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64570 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: 12 hours ago
TLE from 12 hours ago
0 ICEYE-X54
1 64570U 25135AU 25340.91831015 .00007087 00000-0 68793-3 0 9998
2 64570 97.7593 92.6441 0001605 202.8670 157.2478 14.92938804 25196Epoch: 2025-12-06T22:02Z
TLE epoch observation values (Epoch: 2025-12-06T22:02:21.996Z)
Latitude
-0.00007°
Longitude
46.1133°
Altitude
592.853 km
Speed
7.563 km/s
True Right ascension
06h 10m 34s
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
08:11:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
586.913 km
Perigee altitude
584.677 km
Semi-major axis
6,963.932 km
Eccentricity
0.00016
Inclination
97.7593°
RAAN
92.6441°
Arg. of periapsis
202.867°
True anomaly
157.25491°
Mean anomaly
157.2478°
Eccentric anomaly
157.25136°
Mean motion
3.73475 °/min
Orbital period
96.39 mins
BSTAR
0.00068793
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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-X54 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 | 2025-12-07 19:32:55.861Z | 59.905° ENE | 2025-12-07 19:34:55.861Z | 94.558° ESE | 17.776° | 2025-12-07 19:36:55.861Z | 128.765° SE |
| 6 mins | 2025-12-07 21:07:55.861Z | 342.801° N | 2025-12-07 21:10:55.861Z | 273.934° WNW | 27.658° | 2025-12-07 21:13:55.861Z | 226.644° WSW |
| 6 mins | 2025-12-08 07:56:55.861Z | 187.75° SSW | 2025-12-08 07:59:55.861Z | 271.421° WNW | 38.561° | 2025-12-08 08:02:55.861Z | 334.321° 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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