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: 8 hours ago
TLE from 8 hours ago
0 ICEYE-X57
1 64578U 25135BC 26046.26127185 .00005411 00000-0 43640-3 0 9997
2 64578 97.7572 162.6620 0001754 92.8114 267.3310 15.00299485 35737Epoch: 2026-02-15T06:16Z
TLE epoch observation values (Epoch: 2026-02-15T06:16:13.887Z)
Latitude
-0.00006°
Longitude
-76.66837°
Altitude
569.082 km
Speed
7.576 km/s
True Right ascension
10h 50m 38s
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
16:30:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
564.197 km
Perigee altitude
561.762 km
Semi-major axis
6,941.116 km
Eccentricity
0.00018
Inclination
97.7572°
RAAN
162.662°
Arg. of periapsis
92.8114°
True anomaly
267.31092°
Mean anomaly
267.331°
Eccentric anomaly
267.32096°
Mean motion
3.75318 °/min
Orbital period
95.92 mins
BSTAR
0.0004364
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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 | 2026-02-15 19:39:58.725Z | 54.917° ENE | 2026-02-15 19:41:58.725Z | 90.073° ESE | 18.891° | 2026-02-15 19:44:58.725Z | 140.943° SSE |
| 5 mins | 2026-02-15 21:14:58.725Z | 337.615° N | 2026-02-15 21:16:58.725Z | 296.378° NW | 25.419° | 2026-02-15 21:19:58.725Z | 235.73° WSW |
| 6 mins | 2026-02-16 08:00:58.725Z | 191.415° SSW | 2026-02-16 08:02:58.725Z | 236.151° WSW | 36.757° | 2026-02-16 08:06:58.725Z | 335.66° 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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