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: 9 hours ago
TLE from 9 hours ago
0 ICEYE-X57
1 64578U 25135BC 26171.46678061 .00003459 00000-0 27669-3 0 9995
2 64578 97.7955 287.9381 0001964 60.9521 299.1899 15.00873284 54515Epoch: 2026-06-20T11:12Z
TLE epoch observation values (Epoch: 2026-06-20T11:12:09.844Z)
Latitude
-0.00005°
Longitude
-148.7839°
Altitude
566.59 km
Speed
7.578 km/s
True Right ascension
19h 11m 45s
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
07:22:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.573 km
Perigee altitude
559.848 km
Semi-major axis
6,939.347 km
Eccentricity
0.0002
Inclination
97.7955°
RAAN
287.9381°
Arg. of periapsis
60.9521°
True anomaly
299.17025°
Mean anomaly
299.1899°
Eccentric anomaly
299.18008°
Mean motion
3.75461 °/min
Orbital period
95.88 mins
BSTAR
0.00027669
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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 | 2026-06-20 21:22:03.719Z | 343.233° N | 2026-06-20 21:25:03.719Z | 282.001° WNW | 25.356° | 2026-06-20 21:28:03.719Z | 231.246° WSW |
| 6 mins | 2026-06-21 08:08:03.719Z | 189.421° SSW | 2026-06-21 08:11:03.719Z | 278.292° WNW | 37.205° | 2026-06-21 08:14:03.719Z | 334.484° NNW |
| 4 mins | 2026-06-21 19:48:03.719Z | 60.813° ENE | 2026-06-21 19:50:03.719Z | 98.957° ESE | 18.857° | 2026-06-21 19:52:03.719Z | 134.128° SE |
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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