ICEYE-X59, 66752
Orbit data source: Space-Track
ICEYE-X59, 66752 is a Greek payload satellite 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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66752 intel report (Beta)
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Identifier
Orbit
Country
GR / GRECRelated 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: 7 hours ago
TLE from 7 hours ago
0 ICEYE-X59
1 66752U 25276CQ 26144.91667824 -.00149382 00000-0 -12260-1 0 9999
2 66752 97.4246 217.2293 0001939 88.3122 90.5114 15.00038519 5852Epoch: 2026-05-24T22:00Z
TLE epoch observation values (Epoch: 2026-05-24T22:00:00.999Z)
Latitude
1.02974°
Longitude
-175.15335°
Altitude
569.725 km
Speed
7.576 km/s
True Right ascension
02h 29m 27s
True Declination
1° 01' 24"
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
14:11:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
565.117 km
Perigee altitude
562.425 km
Semi-major axis
6,941.908 km
Eccentricity
0.00019
Inclination
97.4246°
RAAN
217.2293°
Arg. of periapsis
88.3122°
True anomaly
90.53362°
Mean anomaly
90.5114°
Eccentric anomaly
90.52251°
Mean motion
3.75254 °/min
Orbital period
95.94 mins
BSTAR
-0.01226
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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-X59 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 | 2026-05-25 05:20:05.288Z | 196.913° SSW | 2026-05-25 05:23:05.288Z | 261.35° W | 32.14° | 2026-05-25 05:26:05.288Z | 326.844° NNW |
| 5 mins | 2026-05-25 17:01:05.288Z | 58.169° ENE | 2026-05-25 17:03:05.288Z | 106.653° ESE | 24.536° | 2026-05-25 17:06:05.288Z | 155.229° SSE |
| 4 mins | 2026-05-25 18:36:05.288Z | 321.871° NNW | 2026-05-25 18:38:05.288Z | 281.373° WNW | 19.489° | 2026-05-25 18:40:05.288Z | 247.972° W |
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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