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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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: 7 hours ago
TLE from 7 hours ago
0 ICEYE-X57
1 64578U 25135BC 26120.26452822 .00004926 00000-0 39195-3 0 9999
2 64578 97.7793 236.6317 0002050 47.7379 312.4018 15.00867079 46839Epoch: 2026-04-30T06:20Z
TLE epoch observation values (Epoch: 2026-04-30T06:20:55.238Z)
Latitude
-0.00003°
Longitude
-76.81208°
Altitude
566.315 km
Speed
7.578 km/s
True Right ascension
15h 46m 31s
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
21:07:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.651 km
Perigee altitude
559.806 km
Semi-major axis
6,939.366 km
Eccentricity
0.00021
Inclination
97.7793°
RAAN
236.6317°
Arg. of periapsis
47.7379°
True anomaly
312.38445°
Mean anomaly
312.4018°
Eccentric anomaly
312.39313°
Mean motion
3.7546 °/min
Orbital period
95.88 mins
BSTAR
0.00039195
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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 | 2026-04-30 19:44:03.214Z | 51.056° ENE | 2026-04-30 19:47:03.214Z | 104.715° ESE | 18.662° | 2026-04-30 19:49:03.214Z | 137.642° SSE |
| 4 mins | 2026-04-30 21:20:03.214Z | 326.364° NNW | 2026-04-30 21:22:03.214Z | 275.967° WNW | 24.848° | 2026-04-30 21:24:03.214Z | 238.701° WSW |
| 6 mins | 2026-05-01 08:05:03.214Z | 191.208° SSW | 2026-05-01 08:07:03.214Z | 234.869° WSW | 36.548° | 2026-05-01 08:11:03.214Z | 335.497° 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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