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: 3 hours ago
TLE from 3 hours ago
0 ICEYE-X57
1 64578U 25135BC 26062.86213383 .00003159 00000-0 25296-3 0 9991
2 64578 97.7613 179.2387 0002044 79.3519 280.7935 15.00886796 38225Epoch: 2026-03-03T20:41Z
TLE epoch observation values (Epoch: 2026-03-03T20:41:28.362Z)
Latitude
-0.00003°
Longitude
67.23542°
Altitude
566.949 km
Speed
7.578 km/s
True Right ascension
11h 56m 57s
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
03:50:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.586 km
Perigee altitude
559.749 km
Semi-major axis
6,939.304 km
Eccentricity
0.0002
Inclination
97.7613°
RAAN
179.2387°
Arg. of periapsis
79.3519°
True anomaly
280.77049°
Mean anomaly
280.7935°
Eccentric anomaly
280.782°
Mean motion
3.75465 °/min
Orbital period
95.88 mins
BSTAR
0.00025296
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-03-04 08:01:45.171Z | 192.563° SSW | 2026-03-04 08:03:45.171Z | 244.24° WSW | 37.48° | 2026-03-04 08:07:45.171Z | 336.444° NNW |
| 4 mins | 2026-03-04 19:41:45.171Z | 67.411° ENE | 2026-03-04 19:42:45.171Z | 86.584° E | 18.713° | 2026-03-04 19:45:45.171Z | 139.164° SSE |
| 5 mins | 2026-03-04 21:15:45.171Z | 339.216° N | 2026-03-04 21:17:45.171Z | 299.974° NW | 25.161° | 2026-03-04 21:20:45.171Z | 237.051° WSW |
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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