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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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, 2.4 m
Radar Cross Section
0.776 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 ICEYE-X56
1 64574U 25135AY 26062.56761001 .00005264 00000-0 48836-3 0 9993
2 64574 97.7613 178.4922 0001330 353.1032 7.0170 14.94853645 38148Epoch: 2026-03-03T13:37Z
TLE epoch observation values (Epoch: 2026-03-03T13:37:21.504Z)
Latitude
-0.00004°
Longitude
172.80779°
Altitude
584.954 km
Speed
7.568 km/s
True Right ascension
11h 53m 58s
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
23:37:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
580.767 km
Perigee altitude
578.916 km
Semi-major axis
6,957.979 km
Eccentricity
0.00013
Inclination
97.7613°
RAAN
178.4922°
Arg. of periapsis
353.1032°
True anomaly
7.01886°
Mean anomaly
7.017°
Eccentric anomaly
7.01793°
Mean motion
3.73954 °/min
Orbital period
96.27 mins
BSTAR
0.00048836
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-03-03 20:36:53.489Z | 8.969° NNE | 2026-03-03 20:39:53.489Z | 335.804° NNW | 43.59° | 2026-03-03 20:43:53.489Z | 198.162° SSW |
| 6 mins | 2026-03-04 07:25:53.489Z | 149.681° SSE | 2026-03-04 07:28:53.489Z | 52.469° ENE | 40.395° | 2026-03-04 07:31:53.489Z | 357.335° N |
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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