ICEYE-X57, 64578
Orbit data source: Space-Track
ICEYE-X57, 64578 is a payload satellite owned by ICEYE US (US) 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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64578 intel report (Beta)
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Identifier
Orbit
Country
USRelated 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: 13 hours ago
TLE from 13 hours ago
0 ICEYE-X57
1 64578U 25135BC 26289.80642013 .00008164 00000-0 64631-3 0 9999
2 64578 97.8290 46.8717 0001831 54.2292 305.9102 15.00863160 72264Epoch: 2026-10-16T19:21Z
TLE epoch observation values (Epoch: 2026-10-16T19:21:14.699Z)
Latitude
0.00004°
Longitude
91.2383°
Altitude
566.54 km
Speed
7.578 km/s
True Right ascension
03h 07m 29s
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
03:08:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.514 km
Perigee altitude
559.973 km
Semi-major axis
6,939.38 km
Eccentricity
0.00018
Inclination
97.829°
RAAN
46.8717°
Arg. of periapsis
54.2292°
True anomaly
305.8932°
Mean anomaly
305.9102°
Eccentric anomaly
305.9017°
Mean motion
3.75459 °/min
Orbital period
95.88 mins
BSTAR
0.00064631
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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-X57 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 | 2026-10-17 19:56:26.556Z | 51.392° ENE | 2026-10-17 19:58:26.556Z | 83.997° E | 19.702° | 2026-10-17 20:01:26.556Z | 137.611° SSE |
| 5 mins | 2026-10-17 21:31:26.556Z | 340.782° N | 2026-10-17 21:33:26.556Z | 303.449° NW | 27.995° | 2026-10-17 21:36:26.556Z | 238.376° WSW |
| 6 mins | 2026-10-18 08:17:26.556Z | 191.503° SSW | 2026-10-18 08:19:26.556Z | 237.827° WSW | 48.997° | 2026-10-18 08:23:26.556Z | 335.811° 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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