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: 12 hours ago
TLE from 12 hours ago
0 ICEYE-X65
1 66300U 25248H 26242.67724095 .00003007 00000-0 20755-3 0 9994
2 66300 45.4042 102.4199 0004060 85.0020 275.1325 15.08131866 46764Epoch: 2026-08-30T16:15Z
TLE epoch observation values (Epoch: 2026-08-30T16:15:13.618Z)
Latitude
-0.00001°
Longitude
-120.25624°
Altitude
541.702 km
Speed
7.593 km/s
True Right ascension
06h 49m 40s
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
19:44:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
546.247 km
Perigee altitude
540.627 km
Semi-major axis
6,921.574 km
Eccentricity
0.00041
Inclination
45.4042°
RAAN
102.4199°
Arg. of periapsis
85.002°
True anomaly
275.08616°
Mean anomaly
275.1325°
Eccentric anomaly
275.10933°
Mean motion
3.76908 °/min
Orbital period
95.51 mins
BSTAR
0.00020755
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-08-31 17:54:52.395Z | 218.708° SW | 2026-08-31 17:56:52.395Z | 152.463° SSE | 40.196° | 2026-08-31 18:00:52.395Z | 70.972° E |
| 6 mins | 2026-08-31 19:34:52.395Z | 284.007° WNW | 2026-08-31 19:36:52.395Z | 336.387° NNW | 35.564° | 2026-08-31 19:40:52.395Z | 61.163° ENE |
| 6 mins | 2026-08-31 21:14:52.395Z | 302.873° NW | 2026-08-31 21:17:52.395Z | 13.762° NNE | 32.012° | 2026-08-31 21:20:52.395Z | 72.616° E |
| 6 mins | 2026-08-31 22:55:52.395Z | 295.946° NW | 2026-08-31 22:57:52.395Z | 313.783° NW | 44.622° | 2026-08-31 23:01:52.395Z | 114.21° SE |
| 4 mins | 2026-09-01 00:35:52.395Z | 255.499° W | 2026-09-01 00:37:52.395Z | 218.268° SW | 19.203° | 2026-09-01 00:39:52.395Z | 182.455° SSW |
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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