ICEYE-X56, 64574
Orbit data source: Space-Track
ICEYE-X56, 64574 is a payload satellite owned by ICEYE (FI) 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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64574 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
FI / FINRelated 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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 ICEYE-X56
1 64574U 25135AY 25328.19510856 .00005091 00000-0 48646-3 0 9993
2 64574 97.7610 80.2604 0000966 322.6496 37.4656 14.93701413 23303Epoch: 2025-11-24T04:40Z
TLE epoch observation values (Epoch: 2025-11-24T04:40:57.379Z)
Latitude
-0.00008°
Longitude
-53.37723°
Altitude
588.917 km
Speed
7.566 km/s
True Right ascension
05h 21m 02s
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
10:44:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
584.095 km
Perigee altitude
582.75 km
Semi-major axis
6,961.56 km
Eccentricity
0.0001
Inclination
97.761°
RAAN
80.2604°
Arg. of periapsis
322.6496°
True anomaly
37.47233°
Mean anomaly
37.4656°
Eccentric anomaly
37.46897°
Mean motion
3.73666 °/min
Orbital period
96.34 mins
BSTAR
0.00048646
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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-X56 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 | 2025-11-24 19:44:13.917Z | 46.562° ENE | 2025-11-24 19:47:13.917Z | 103.205° ESE | 22.549° | 2025-11-24 19:50:13.917Z | 150.763° SSE |
| 5 mins | 2025-11-24 21:20:13.917Z | 331.483° NNW | 2025-11-24 21:22:13.917Z | 291.644° WNW | 22.784° | 2025-11-24 21:25:13.917Z | 239.385° WSW |
| 5 mins | 2025-11-25 08:09:13.917Z | 206.4° SW | 2025-11-25 08:11:13.917Z | 257.305° W | 32.176° | 2025-11-25 08:14:13.917Z | 325.048° 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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