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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 4 hours ago
TLE from 4 hours ago
0 ICEYE-X56
1 64574U 25135AY 26193.18625450 .00001882 00000-0 17406-3 0 9994
2 64574 97.7762 307.9524 0001157 208.4427 151.6731 14.95750241 57663Epoch: 2026-07-12T04:28Z
TLE epoch observation values (Epoch: 2026-07-12T04:28:12.388Z)
Latitude
-0.00003°
Longitude
-49.18795°
Altitude
583.8 km
Speed
7.568 km/s
True Right ascension
20h 31m 48s
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
21:05:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
577.864 km
Perigee altitude
576.255 km
Semi-major axis
6,955.196 km
Eccentricity
0.00012
Inclination
97.7762°
RAAN
307.9524°
Arg. of periapsis
208.4427°
True anomaly
151.67939°
Mean anomaly
151.6731°
Eccentric anomaly
151.67625°
Mean motion
3.74179 °/min
Orbital period
96.21 mins
BSTAR
0.00017406
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-07-12 19:30:41.101Z | 57.158° ENE | 2026-07-12 19:32:41.101Z | 87.299° E | 14.909° | 2026-07-12 19:34:41.101Z | 120.23° SE |
| 6 mins | 2026-07-12 21:05:41.101Z | 349.307° N | 2026-07-12 21:08:41.101Z | 279.138° WNW | 31.655° | 2026-07-12 21:11:41.101Z | 222.89° SW |
| 7 mins | 2026-07-13 07:52:41.101Z | 175.98° S | 2026-07-13 07:56:41.101Z | 276.723° WNW | 42.363° | 2026-07-13 07:59:41.101Z | 339.719° 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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