ICEYE-X67, 66302
Orbit data source: Space-Track
ICEYE-X67, 66302 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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66302 intel report (Beta)
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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: 12 hours ago
TLE from 12 hours ago
0 ICEYE-X67
1 66302U 25248K 26242.66149784 .00002945 00000-0 19697-3 0 9994
2 66302 45.4045 100.6965 0005206 82.0395 278.1077 15.09372650 46772Epoch: 2026-08-30T15:52Z
TLE epoch observation values (Epoch: 2026-08-30T15:52:33.413Z)
Latitude
-0.00008°
Longitude
-116.29667°
Altitude
537.653 km
Speed
7.596 km/s
True Right ascension
06h 42m 47s
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
19:43:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
543.246 km
Perigee altitude
536.043 km
Semi-major axis
6,917.782 km
Eccentricity
0.00052
Inclination
45.4045°
RAAN
100.6965°
Arg. of periapsis
82.0395°
True anomaly
278.04863°
Mean anomaly
278.1077°
Eccentric anomaly
278.07817°
Mean motion
3.77218 °/min
Orbital period
95.44 mins
BSTAR
0.00019697
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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-X67 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 | 2026-08-31 17:29:16.616Z | 213.536° SW | 2026-08-31 17:32:16.616Z | 143.293° SSE | 34.427° | 2026-08-31 17:35:16.616Z | 79.015° E |
| 6 mins | 2026-08-31 19:09:16.616Z | 270.763° WNW | 2026-08-31 19:12:16.616Z | 350.254° N | 38.392° | 2026-08-31 19:15:16.616Z | 58.07° ENE |
| 6 mins | 2026-08-31 20:50:16.616Z | 305.006° NW | 2026-08-31 20:52:16.616Z | 349.186° N | 30.643° | 2026-08-31 20:56:16.616Z | 71.058° E |
| 6 mins | 2026-08-31 22:30:16.616Z | 299.773° NW | 2026-08-31 22:33:16.616Z | 52.352° ENE | 42.79° | 2026-08-31 22:36:16.616Z | 104.623° ESE |
| 4 mins | 2026-09-01 00:11:16.616Z | 253.033° W | 2026-09-01 00:13:16.616Z | 204.591° SW | 23.871° | 2026-09-01 00:15:16.616Z | 168.077° S |
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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