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 26295.40779107 .00003229 00000-0 21303-3 0 9995
2 66302 45.4032 182.6456 0005797 4.8428 355.2509 15.09618079 54748Epoch: 2026-10-22T09:47Z
TLE epoch observation values (Epoch: 2026-10-22T09:47:13.148Z)
Latitude
-0.00005°
Longitude
4.99764°
Altitude
533.415 km
Speed
7.6 km/s
True Right ascension
12h 10m 34s
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
16:25:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
542.905 km
Perigee altitude
534.886 km
Semi-major axis
6,917.033 km
Eccentricity
0.00058
Inclination
45.4032°
RAAN
182.6456°
Arg. of periapsis
4.8428°
True anomaly
355.2454°
Mean anomaly
355.2509°
Eccentric anomaly
355.24815°
Mean motion
3.7728 °/min
Orbital period
95.42 mins
BSTAR
0.00021303
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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 | 2026-10-22 22:50:14.067Z | 296.157° NW | 2026-10-22 22:53:14.067Z | 357.525° N | 36.728° | 2026-10-22 22:56:14.067Z | 62.525° ENE |
| 6 mins | 2026-10-23 00:31:14.067Z | 304.395° NW | 2026-10-23 00:33:14.067Z | 344.438° N | 54.38° | 2026-10-23 00:37:14.067Z | 97.798° ESE |
| 6 mins | 2026-10-23 02:11:14.067Z | 270.646° WNW | 2026-10-23 02:13:14.067Z | 227.871° WSW | 34.606° | 2026-10-23 02:17:14.067Z | 149.643° SSE |
| 6 mins | 2026-10-23 19:20:14.067Z | 212.417° SW | 2026-10-23 19:23:14.067Z | 136.889° SSE | 43.049° | 2026-10-23 19:26:14.067Z | 78.04° E |
| 6 mins | 2026-10-23 21:00:14.067Z | 271.829° WNW | 2026-10-23 21:03:14.067Z | 359.144° N | 51.44° | 2026-10-23 21:06:14.067Z | 58.497° ENE |
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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