ICEYE-X60, 66753
Orbit data source: Space-Track
ICEYE-X60, 66753 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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66753 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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 ICEYE-X60
1 66753U 25276CR 26191.63057498 .00002984 00000-0 18050-3 0 9990
2 66753 97.4184 263.6173 0000894 208.4786 151.6396 15.11381751 33905Epoch: 2026-07-10T15:08Z
TLE epoch observation values (Epoch: 2026-07-10T15:08:01.678Z)
Latitude
0.00002°
Longitude
108.05492°
Altitude
535.607 km
Speed
7.594 km/s
True Right ascension
17h 34m 28s
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
17:09:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
529.581 km
Perigee altitude
528.346 km
Semi-major axis
6,907.1 km
Eccentricity
0.00009
Inclination
97.4184°
RAAN
263.6173°
Arg. of periapsis
208.4786°
True anomaly
151.64447°
Mean anomaly
151.6396°
Eccentric anomaly
151.64203°
Mean motion
3.78094 °/min
Orbital period
95.21 mins
BSTAR
0.0001805
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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-X60 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 | 2026-07-12 05:23:32.763Z | 199.226° SSW | 2026-07-12 05:26:32.763Z | 264.328° W | 29.907° | 2026-07-12 05:29:32.763Z | 326.342° NNW |
| 4 mins | 2026-07-12 16:59:32.763Z | 66.1° ENE | 2026-07-12 17:00:32.763Z | 89.071° E | 21.972° | 2026-07-12 17:03:32.763Z | 147.002° SSE |
| 4 mins | 2026-07-12 18:33:32.763Z | 322.748° NNW | 2026-07-12 18:35:32.763Z | 279.184° WNW | 19.929° | 2026-07-12 18:37:32.763Z | 244.623° WSW |
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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