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: 22 hours ago
TLE from 22 hours ago
0 ICEYE-X6
1 46497U 20068M 26172.51429503 .00002136 00000-0 15710-3 0 9992
2 46497 98.0984 166.3926 0009048 79.2813 280.9430 15.04545583313883Epoch: 2026-06-21T12:20Z
TLE epoch observation values (Epoch: 2026-06-21T12:20:35.090Z)
Latitude
-0.00003°
Longitude
71.53292°
Altitude
554.764 km
Speed
7.585 km/s
True Right ascension
11h 05m 34s
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
21:36:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
556.187 km
Perigee altitude
543.65 km
Semi-major axis
6,928.055 km
Eccentricity
0.0009
Inclination
98.0984°
RAAN
166.3926°
Arg. of periapsis
79.2813°
True anomaly
280.84118°
Mean anomaly
280.943°
Eccentric anomaly
280.89209°
Mean motion
3.7638 °/min
Orbital period
95.65 mins
BSTAR
0.0001571
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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 | 2026-06-22 12:51:31.783Z | 354.7° N | 2026-06-22 12:53:31.783Z | 308.985° NW | 36.879° | 2026-06-22 12:57:31.783Z | 211.424° SW |
| 6 mins | 2026-06-22 23:35:31.783Z | 163.737° S | 2026-06-22 23:38:31.783Z | 5.037° NNE | 44.029° | 2026-06-22 23:41:31.783Z | 348.562° 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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