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: 12 hours ago
TLE from 12 hours ago
0 ICEYE-X57
1 64578U 25135BC 26259.93800985 .00003963 00000-0 31644-3 0 9994
2 64578 97.8200 16.8026 0001894 50.2557 309.8833 15.00858782 67783Epoch: 2026-09-16T22:30Z
TLE epoch observation values (Epoch: 2026-09-16T22:30:44.051Z)
Latitude
-0.00001°
Longitude
43.23663°
Altitude
566.456 km
Speed
7.578 km/s
True Right ascension
01h 07m 12s
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
03:01:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.571 km
Perigee altitude
559.942 km
Semi-major axis
6,939.393 km
Eccentricity
0.00019
Inclination
97.82°
RAAN
16.8026°
Arg. of periapsis
50.2557°
True anomaly
309.86664°
Mean anomaly
309.8833°
Eccentric anomaly
309.87497°
Mean motion
3.75458 °/min
Orbital period
95.88 mins
BSTAR
0.00031644
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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 | 2026-09-17 19:53:50.539Z | 50.329° ENE | 2026-09-17 19:56:50.539Z | 103.07° ESE | 19.87° | 2026-09-17 19:58:50.539Z | 136.564° SSE |
| 5 mins | 2026-09-17 21:29:50.539Z | 327.855° NNW | 2026-09-17 21:31:50.539Z | 277.968° WNW | 28.173° | 2026-09-17 21:34:50.539Z | 230.135° WSW |
| 6 mins | 2026-09-18 08:14:50.539Z | 190.711° SSW | 2026-09-18 08:16:50.539Z | 233.054° WSW | 47.849° | 2026-09-18 08:20:50.539Z | 335.396° 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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