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: 7 hours ago
TLE from 7 hours ago
0 ICEYE-X55
1 64581U 25135BF 26062.53869017 .00006409 00000-0 59972-3 0 9999
2 64581 97.7617 178.3751 0002583 8.6693 351.4571 14.94432651 38135Epoch: 2026-03-03T12:55Z
TLE epoch observation values (Epoch: 2026-03-03T12:55:42.830Z)
Latitude
-0.00007°
Longitude
-176.86966°
Altitude
585.401 km
Speed
7.569 km/s
True Right ascension
11h 53m 30s
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
23:39:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
582.947 km
Perigee altitude
579.352 km
Semi-major axis
6,959.287 km
Eccentricity
0.00026
Inclination
97.7617°
RAAN
178.3751°
Arg. of periapsis
8.6693°
True anomaly
351.4527°
Mean anomaly
351.4571°
Eccentric anomaly
351.4549°
Mean motion
3.73849 °/min
Orbital period
96.3 mins
BSTAR
0.00059972
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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 | 2026-03-03 19:56:06.959Z | 38.087° NE | 2026-03-03 19:59:06.959Z | 98.886° ESE | 28.595° | 2026-03-03 20:02:06.959Z | 157.463° SSE |
| 4 mins | 2026-03-04 06:46:06.959Z | 102.008° ESE | 2026-03-04 06:48:06.959Z | 63.738° ENE | 19.788° | 2026-03-04 06:50:06.959Z | 28.56° NE |
| 5 mins | 2026-03-04 08:21:06.959Z | 218.381° SW | 2026-03-04 08:23:06.959Z | 262.911° W | 25.921° | 2026-03-04 08:26:06.959Z | 319.686° 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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