ICEYE-X66, 66301
Orbit data source: Space-Track
ICEYE-X66, 66301 is an Emirian payload satellite in LEO that was launched on Sun, 02 Nov 2025 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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Identifier
Orbit
Country
AE / UAERelated business
None
Manufacturer
SP42
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: 1 day ago
TLE from 1 day ago
0 ICEYE-X66
1 66301U 25248J 26241.97431638 .00001897 00000-0 13237-3 0 9997
2 66301 45.3989 104.7165 0004202 73.2246 286.9096 15.09398707 46652Epoch: 2026-08-29T23:23Z
TLE epoch observation values (Epoch: 2026-08-29T23:23:00.935Z)
Latitude
-0.00007°
Longitude
135.78597°
Altitude
537.235 km
Speed
7.596 km/s
True Right ascension
06h 58m 51s
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
19:43:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
542.473 km
Perigee altitude
536.659 km
Semi-major axis
6,917.703 km
Eccentricity
0.00042
Inclination
45.3989°
RAAN
104.7165°
Arg. of periapsis
73.2246°
True anomaly
286.86352°
Mean anomaly
286.9096°
Eccentric anomaly
286.88656°
Mean motion
3.77225 °/min
Orbital period
95.43 mins
BSTAR
0.00013237
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Other satellites on launch #248 in the year 2025 (2025-11-02 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-X66 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 | 2026-08-31 16:51:21.265Z | 188.293° SSW | 2026-08-31 16:54:21.265Z | 133.31° SE | 21.022° | 2026-08-31 16:56:21.265Z | 97.366° ESE |
| 6 mins | 2026-08-31 18:31:21.265Z | 251.586° W | 2026-08-31 18:33:21.265Z | 278.066° WNW | 43.393° | 2026-08-31 18:37:21.265Z | 63.925° ENE |
| 6 mins | 2026-08-31 20:11:21.265Z | 293.399° NW | 2026-08-31 20:14:21.265Z | 7.045° NNE | 31.245° | 2026-08-31 20:17:21.265Z | 61.862° ENE |
| 6 mins | 2026-08-31 21:52:21.265Z | 309.659° NW | 2026-08-31 21:54:21.265Z | 4.557° NNE | 36.612° | 2026-08-31 21:58:21.265Z | 89.651° E |
| 6 mins | 2026-08-31 23:32:21.265Z | 278.067° WNW | 2026-08-31 23:34:21.265Z | 224.676° SW | 37.673° | 2026-08-31 23:38:21.265Z | 136.086° SSE |
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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