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 26120.21643218 .00003426 00000-0 32445-3 0 9992
2 64570 97.7666 235.1343 0003734 107.0117 253.1513 14.94274895 46733Epoch: 2026-04-30T05:11Z
TLE epoch observation values (Epoch: 2026-04-30T05:11:39.740Z)
Latitude
0.00004°
Longitude
-60.94751°
Altitude
588.424 km
Speed
7.566 km/s
True Right ascension
15h 40m 32s
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
19:56:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
584.239 km
Perigee altitude
579.041 km
Semi-major axis
6,959.777 km
Eccentricity
0.00037
Inclination
97.7666°
RAAN
235.1343°
Arg. of periapsis
107.0117°
True anomaly
253.11035°
Mean anomaly
253.1513°
Eccentric anomaly
253.13083°
Mean motion
3.73809 °/min
Orbital period
96.31 mins
BSTAR
0.00032445
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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 | 2026-04-30 20:13:27.837Z | 23.198° NE | 2026-04-30 20:17:27.837Z | 125.95° SE | 38.208° | 2026-04-30 20:20:27.837Z | 176.579° S |
| 5 mins | 2026-05-01 07:03:27.837Z | 123.361° SE | 2026-05-01 07:05:27.837Z | 81.352° E | 28.23° | 2026-05-01 07:08:27.837Z | 15.101° NNE |
| 4 mins | 2026-05-01 08:39:27.837Z | 234.918° WSW | 2026-05-01 08:41:27.837Z | 270.233° WNW | 17.376° | 2026-05-01 08:43:27.837Z | 303.203° NW |
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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