ICEYE-X6, 46497
Orbit data source: Space-Track
ICEYE-X6, 46497 is a payload satellite owned by ICEYE (FI) in SSO that was launched on Mon, 28 Sep 2020 UTC via a SOYUZ-2-1B launch vehicle from the Plesetsk Missile And Space Complex (PKMTR). 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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46497 intel report (Beta)
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Identifier
Orbit
Country
FI / FINRelated business
Manufacturer
ICEYE
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
1.837 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 ICEYE-X6
1 46497U 20068M 26080.91917850 .00004638 00000-0 34046-3 0 9993
2 46497 98.0952 70.4678 0007953 31.3218 328.8478 15.03981365300115Epoch: 2026-03-21T22:03Z
TLE epoch observation values (Epoch: 2026-03-21T22:03:37.022Z)
Latitude
-0.00009°
Longitude
-79.86943°
Altitude
552.964 km
Speed
7.588 km/s
True Right ascension
04h 41m 52s
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
12:05:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
557.163 km
Perigee altitude
546.141 km
Semi-major axis
6,929.789 km
Eccentricity
0.0008
Inclination
98.0952°
RAAN
70.4678°
Arg. of periapsis
31.3218°
True anomaly
328.80061°
Mean anomaly
328.8478°
Eccentric anomaly
328.82421°
Mean motion
3.76238 °/min
Orbital period
95.68 mins
BSTAR
0.00034046
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Other satellites on launch #68 in the year 2020 (2020-09-28 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-X6 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 | 2026-03-22 11:24:48.607Z | 45.087° ENE | 2026-03-22 11:27:48.607Z | 103.519° ESE | 22.94° | 2026-03-22 11:30:48.607Z | 153.018° SSE |
| 4 mins | 2026-03-22 13:00:48.607Z | 320.836° NNW | 2026-03-22 13:01:48.607Z | 300.118° NW | 20.744° | 2026-03-22 13:04:48.607Z | 244.335° WSW |
| 5 mins | 2026-03-22 23:44:48.607Z | 205.68° SW | 2026-03-22 23:46:48.607Z | 257.416° W | 31.347° | 2026-03-22 23:49:48.607Z | 325.153° NNW |
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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