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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Edit Public Description
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, 1.6 m
Radar Cross Section
1.837 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 ICEYE-X6
1 46497U 20068M 25358.27535404 .00003680 00000-0 27687-3 0 9999
2 46497 98.0865 338.8831 0006181 331.6601 28.4286 15.03206774286942Epoch: 2025-12-24T06:36Z
TLE epoch observation values (Epoch: 2025-12-24T06:36:30.589Z)
Latitude
0.00001°
Longitude
146.70856°
Altitude
556.293 km
Speed
7.586 km/s
True Right ascension
22h 35m 31s
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
10:46:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
558.319 km
Perigee altitude
549.749 km
Semi-major axis
6,932.171 km
Eccentricity
0.00062
Inclination
98.0865°
RAAN
338.8831°
Arg. of periapsis
331.6601°
True anomaly
28.46234°
Mean anomaly
28.4286°
Eccentric anomaly
28.44547°
Mean motion
3.76045 °/min
Orbital period
95.73 mins
BSTAR
0.00027687
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-12-24 11:57:37.575Z | 6.407° NNE | 2025-12-24 12:00:37.575Z | 328.162° NNW | 41.078° | 2025-12-24 12:04:37.575Z | 203.341° SW |
| 6 mins | 2025-12-24 22:43:37.575Z | 151.393° SSE | 2025-12-24 22:45:37.575Z | 102.288° ESE | 41.762° | 2025-12-24 22:49:37.575Z | 353.554° N |
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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