ICEYE-X58, 66751
Orbit data source: Space-Track
ICEYE-X58, 66751 is a payload satellite owned by ICEYE (FI) in SSO that was launched on Fri, 28 Nov 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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66751 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
120 kg wet, 120 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
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 ICEYE-X58
1 66751U 25276CP 26141.15712013 .00002037 00000-0 10439-3 0 9993
2 66751 97.4209 215.1336 0004890 80.3100 279.8686 15.17693731 26313Epoch: 2026-05-21T03:46Z
TLE epoch observation values (Epoch: 2026-05-21T03:46:15.179Z)
Latitude
-0.00001°
Longitude
-80.236°
Altitude
515.323 km
Speed
7.606 km/s
True Right ascension
14h 20m 32s
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
01:44:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
513.15 km
Perigee altitude
506.414 km
Semi-major axis
6,887.919 km
Eccentricity
0.00049
Inclination
97.4209°
RAAN
215.1336°
Arg. of periapsis
80.31°
True anomaly
279.81339°
Mean anomaly
279.8686°
Eccentric anomaly
279.84099°
Mean motion
3.79674 °/min
Orbital period
94.82 mins
BSTAR
0.00010439
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Other satellites on launch #276 in the year 2025 (2025-11-28 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-X58 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-05-21 17:00:28.378Z | 48.52° ENE | 2026-05-21 17:02:28.378Z | 84.092° E | 19.535° | 2026-05-21 17:05:28.378Z | 142.485° SSE |
| 4 mins | 2026-05-21 18:35:28.378Z | 321.597° NNW | 2026-05-21 18:36:28.378Z | 299.54° NW | 20.921° | 2026-05-21 18:39:28.378Z | 240.405° WSW |
| 5 mins | 2026-05-22 05:13:28.378Z | 187.37° SSW | 2026-05-22 05:15:28.378Z | 238.774° WSW | 38.935° | 2026-05-22 05:18:28.378Z | 335.166° 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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