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: 14 hours ago
TLE from 14 hours ago
0 ICEYE-X66
1 66301U 25248J 26171.28057961 .00001501 00000-0 10908-3 0 9990
2 66301 45.4017 117.2466 0004485 32.8404 327.2756 15.09001875 35970Epoch: 2026-06-20T06:44Z
TLE epoch observation values (Epoch: 2026-06-20T06:44:02.078Z)
Latitude
-0.00001°
Longitude
107.74046°
Altitude
536.682 km
Speed
7.597 km/s
True Right ascension
07h 48m 59s
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
07:17:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
543.881 km
Perigee altitude
537.675 km
Semi-major axis
6,918.915 km
Eccentricity
0.00045
Inclination
45.4017°
RAAN
117.2466°
Arg. of periapsis
32.8404°
True anomaly
327.2478°
Mean anomaly
327.2756°
Eccentric anomaly
327.2617°
Mean motion
3.77126 °/min
Orbital period
95.46 mins
BSTAR
0.00010908
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-20 22:47:20.953Z | 193.05° SSW | 2026-06-20 22:50:20.953Z | 143.422° SSE | 21.529° | 2026-06-20 22:53:20.953Z | 90.815° ESE |
| 6 mins | 2026-06-21 00:27:20.953Z | 251.277° W | 2026-06-21 00:30:20.953Z | 13.074° NNE | 44.168° | 2026-06-21 00:33:20.953Z | 63.116° ENE |
| 5 mins | 2026-06-21 02:08:20.953Z | 299.164° NW | 2026-06-21 02:10:20.953Z | 348.264° N | 31.486° | 2026-06-21 02:13:20.953Z | 58.149° ENE |
| 6 mins | 2026-06-21 03:48:20.953Z | 304.952° NW | 2026-06-21 03:51:20.953Z | 30.18° NE | 36.536° | 2026-06-21 03:54:20.953Z | 87.603° E |
| 6 mins | 2026-06-21 05:28:20.953Z | 281.871° WNW | 2026-06-21 05:31:20.953Z | 198.78° SSW | 37.364° | 2026-06-21 05:34:20.953Z | 139.043° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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