ICEYE-X60, 66753
Orbit data source: Space-Track
ICEYE-X60, 66753 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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66753 intel report (Beta)
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Edit Public Description
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, 0.8 m
Radar Cross Section
0.776 m²
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 ICEYE-X60
1 66753U 25276CR 26034.15899768 .00004297 00000-0 21569-3 0 9995
2 66753 97.4343 109.9941 0004004 115.1611 245.0038 15.17825944 10072Epoch: 2026-02-03T03:48Z
TLE epoch observation values (Epoch: 2026-02-03T03:48:57.399Z)
Latitude
-0.00008°
Longitude
-80.58899°
Altitude
516.666 km
Speed
7.605 km/s
True Right ascension
07h 19m 58s
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
07:05:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
512.14 km
Perigee altitude
506.625 km
Semi-major axis
6,887.519 km
Eccentricity
0.0004
Inclination
97.4343°
RAAN
109.9941°
Arg. of periapsis
115.1611°
True anomaly
244.96222°
Mean anomaly
245.0038°
Eccentric anomaly
244.98301°
Mean motion
3.79707 °/min
Orbital period
94.81 mins
BSTAR
0.00021569
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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 | 2026-02-04 05:15:40.878Z | 186.495° SSW | 2026-02-04 05:18:40.878Z | 284.129° WNW | 37.817° | 2026-02-04 05:21:40.878Z | 337.308° NNW |
| 5 mins | 2026-02-04 18:21:40.878Z | 340.219° N | 2026-02-04 18:23:40.878Z | 288.568° WNW | 28.987° | 2026-02-04 18:26:40.878Z | 225.132° WSW |
| 5 mins | 2026-02-05 05:00:40.878Z | 167.933° S | 2026-02-05 05:02:40.878Z | 342.169° N | 44.436° | 2026-02-05 05:05:40.878Z | 347.725° N |
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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