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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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: 7 hours ago
TLE from 7 hours ago
0 ICEYE-X54
1 64570U 25135AU 26062.55316747 .00004719 00000-0 44989-3 0 9990
2 64570 97.7598 178.1424 0001125 329.1216 30.9937 14.93828877 38121Epoch: 2026-03-03T13:16Z
TLE epoch observation values (Epoch: 2026-03-03T13:16:33.669Z)
Latitude
-0.00007°
Longitude
177.67155°
Altitude
588.383 km
Speed
7.566 km/s
True Right ascension
11h 52m 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
23:38:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
583.809 km
Perigee altitude
582.243 km
Semi-major axis
6,961.163 km
Eccentricity
0.00011
Inclination
97.7598°
RAAN
178.1424°
Arg. of periapsis
329.1216°
True anomaly
31.00034°
Mean anomaly
30.9937°
Eccentric anomaly
30.99702°
Mean motion
3.73698 °/min
Orbital period
96.33 mins
BSTAR
0.00044989
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-03-03 20:16:40.048Z | 22.253° NNE | 2026-03-03 20:19:40.048Z | 81.199° E | 40.765° | 2026-03-03 20:23:40.048Z | 180.963° SSW |
| 5 mins | 2026-03-04 07:06:40.048Z | 124.54° SE | 2026-03-04 07:08:40.048Z | 76.769° E | 30.55° | 2026-03-04 07:11:40.048Z | 11.435° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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