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: 15 hours ago
TLE from 15 hours ago
0 ICEYE-X57
1 64578U 25135BC 26224.60273465 .00002154 00000-0 17419-3 0 9992
2 64578 97.8099 341.2781 0002075 49.6331 310.5073 15.00865071 62482Epoch: 2026-08-12T14:27Z
TLE epoch observation values (Epoch: 2026-08-12T14:27:56.273Z)
Latitude
-0.00009°
Longitude
163.23934°
Altitude
566.344 km
Speed
7.578 km/s
True Right ascension
22h 45m 06s
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
20:05:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.676 km
Perigee altitude
559.797 km
Semi-major axis
6,939.373 km
Eccentricity
0.00021
Inclination
97.8099°
RAAN
341.2781°
Arg. of periapsis
49.6331°
True anomaly
310.48922°
Mean anomaly
310.5073°
Eccentric anomaly
310.49826°
Mean motion
3.75459 °/min
Orbital period
95.88 mins
BSTAR
0.00017419
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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 | 2026-08-13 08:12:12.817Z | 192.407° SSW | 2026-08-13 08:14:12.817Z | 242.77° WSW | 37.298° | 2026-08-13 08:18:12.817Z | 336.191° NNW |
| 4 mins | 2026-08-13 19:52:12.817Z | 66.793° ENE | 2026-08-13 19:53:12.817Z | 85.746° E | 18.611° | 2026-08-13 19:56:12.817Z | 138.604° SSE |
| 5 mins | 2026-08-13 21:26:12.817Z | 339.873° N | 2026-08-13 21:28:12.817Z | 301.205° NW | 25.203° | 2026-08-13 21:31:12.817Z | 237.4° 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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