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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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: 8 hours ago
TLE from 8 hours ago
0 ICEYE-X55
1 64581U 25135BF 26112.14537167 .00002507 00000-0 23531-3 0 9997
2 64581 97.7673 227.4592 0003858 152.1073 208.0355 14.94865144 45546Epoch: 2026-04-22T03:29Z
TLE epoch observation values (Epoch: 2026-04-22T03:29:20.112Z)
Latitude
-0°
Longitude
-35.0856°
Altitude
588.208 km
Speed
7.565 km/s
True Right ascension
15h 09m 50s
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
18:27:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
582.491 km
Perigee altitude
577.122 km
Semi-major axis
6,957.943 km
Eccentricity
0.00039
Inclination
97.7673°
RAAN
227.4592°
Arg. of periapsis
152.1073°
True anomaly
208.01473°
Mean anomaly
208.0355°
Eccentric anomaly
208.02511°
Mean motion
3.73957 °/min
Orbital period
96.27 mins
BSTAR
0.00023531
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-04-22 20:07:53.450Z | 31.439° NE | 2026-04-22 20:10:53.450Z | 102.112° ESE | 34.902° | 2026-04-22 20:13:53.450Z | 167.638° S |
| 4 mins | 2026-04-23 06:57:53.450Z | 104.319° ESE | 2026-04-23 06:58:53.450Z | 82.482° E | 24.148° | 2026-04-23 07:01:53.450Z | 20.569° NNE |
| 5 mins | 2026-04-23 08:32:53.450Z | 229.738° WSW | 2026-04-23 08:34:53.450Z | 269.124° W | 20.621° | 2026-04-23 08:37:53.450Z | 316.717° 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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