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: 11 hours ago
TLE from 11 hours ago
0 ICEYE-X65
1 66300U 25248H 26295.40102788 .00003011 00000-0 20652-3 0 9993
2 66300 45.4040 185.0216 0004718 4.6055 355.4869 15.08361912 54721Epoch: 2026-10-22T09:37Z
TLE epoch observation values (Epoch: 2026-10-22T09:37:28.808Z)
Latitude
-0.00007°
Longitude
9.81504°
Altitude
537.994 km
Speed
7.597 km/s
True Right ascension
12h 20m 05s
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
15:29:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
545.999 km
Perigee altitude
539.468 km
Semi-major axis
6,920.871 km
Eccentricity
0.00047
Inclination
45.404°
RAAN
185.0216°
Arg. of periapsis
4.6055°
True anomaly
355.48264°
Mean anomaly
355.4869°
Eccentric anomaly
355.48477°
Mean motion
3.76966 °/min
Orbital period
95.5 mins
BSTAR
0.00020652
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-10-22 20:59:12.959Z | 252.537° W | 2026-10-22 21:03:12.959Z | 29.314° NE | 65.603° | 2026-10-22 21:06:12.959Z | 62.483° ENE |
| 5 mins | 2026-10-22 22:41:12.959Z | 303.279° NW | 2026-10-22 22:43:12.959Z | 356.366° N | 37.626° | 2026-10-22 22:46:12.959Z | 59.892° ENE |
| 6 mins | 2026-10-23 00:21:12.959Z | 306.256° NW | 2026-10-23 00:24:12.959Z | 38.595° NE | 47.794° | 2026-10-23 00:27:12.959Z | 89.586° E |
| 6 mins | 2026-10-23 02:01:12.959Z | 279.957° WNW | 2026-10-23 02:04:12.959Z | 194.764° SSW | 46.667° | 2026-10-23 02:07:12.959Z | 140.656° SSE |
| 5 mins | 2026-10-23 19:12:12.959Z | 191.885° SSW | 2026-10-23 19:14:12.959Z | 143.214° SSE | 32.669° | 2026-10-23 19:17:12.959Z | 84.438° E |
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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