ICEYE-X55, 64581
Orbit data source: Space-Track
ICEYE-X55, 64581 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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64581 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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 4 days ago
TLE from 4 days ago
0 ICEYE-X55
1 64581U 25135BF 25324.72138822 .00080058 34897-5 12530-2 0 9999
2 64581 98.5814 73.8170 0384016 13.2384 347.8576 14.99799562 22780Epoch: 2025-11-20T17:18Z
TLE epoch observation values (Epoch: 2025-11-20T17:18:47.942Z)
Latitude
-0.00002°
Longitude
114.14254°
Altitude
310.213 km
Speed
7.865 km/s
True Right ascension
04h 55m 16s
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
15:50:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
831.166 km
Perigee altitude
297.945 km
Semi-major axis
6,942.692 km
Eccentricity
0.0384
Inclination
98.5814°
RAAN
73.817°
Arg. of periapsis
13.2384°
True anomaly
346.88656°
Mean anomaly
347.8576°
Eccentric anomaly
347.37676°
Mean motion
3.7519 °/min
Orbital period
95.95 mins
BSTAR
0.001253
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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-X55 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 | 2025-11-24 19:31:18.792Z | 45.922° ENE | 2025-11-24 19:34:18.792Z | 91.65° ESE | 25.193° | 2025-11-24 19:38:18.792Z | 150.662° SSE |
| 7 mins | 2025-11-24 21:06:18.792Z | 345.439° N | 2025-11-24 21:09:18.792Z | 292.289° WNW | 29.877° | 2025-11-24 21:13:18.792Z | 230.242° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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