ICEYE-X65, 66300
Orbit data source: Space-Track
ICEYE-X65, 66300 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-X65
1 66300U 25248H 26171.26228576 .00001361 00000-0 10369-3 0 9994
2 66300 45.4049 118.0019 0004681 39.6151 320.5072 15.07761391 35981Epoch: 2026-06-20T06:17Z
TLE epoch observation values (Epoch: 2026-06-20T06:17:41.489Z)
Latitude
-0.00002°
Longitude
115.09957°
Altitude
540.586 km
Speed
7.595 km/s
True Right ascension
07h 52m 00s
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
07:18:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
547.811 km
Perigee altitude
541.33 km
Semi-major axis
6,922.707 km
Eccentricity
0.00047
Inclination
45.4049°
RAAN
118.0019°
Arg. of periapsis
39.6151°
True anomaly
320.47307°
Mean anomaly
320.5072°
Eccentric anomaly
320.49014°
Mean motion
3.76816 °/min
Orbital period
95.54 mins
BSTAR
0.00010369
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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-X65 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-20 22:21:39.536Z | 168.426° S | 2026-06-20 22:23:39.536Z | 138.406° SSE | 13.811° | 2026-06-20 22:25:39.536Z | 107.579° ESE |
| 6 mins | 2026-06-21 00:00:39.536Z | 232.725° WSW | 2026-06-21 00:03:39.536Z | 113.97° SE | 42.59° | 2026-06-21 00:06:39.536Z | 69.43° E |
| 5 mins | 2026-06-21 01:41:39.536Z | 292.683° NW | 2026-06-21 01:43:39.536Z | 351.17° N | 34.063° | 2026-06-21 01:46:39.536Z | 57.365° ENE |
| 6 mins | 2026-06-21 03:21:39.536Z | 305.875° NW | 2026-06-21 03:24:39.536Z | 25.528° NE | 32.676° | 2026-06-21 03:27:39.536Z | 78.087° E |
| 7 mins | 2026-06-21 05:01:39.536Z | 291.663° WNW | 2026-06-21 05:04:39.536Z | 191.619° SSW | 44.384° | 2026-06-21 05:08:39.536Z | 121.063° SE |
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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