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: 4 hours ago
TLE from 4 hours ago
0 ICEYE-X6
1 46497U 20068M 26005.19014029 .00004016 00000-0 30072-3 0 9991
2 46497 98.0845 351.3193 0005969 278.8338 81.2210 15.03324197288736Epoch: 2026-01-05T04:33Z
TLE epoch observation values (Epoch: 2026-01-05T04:33:48.121Z)
Latitude
-0.00001°
Longitude
178.07794°
Altitude
559.073 km
Speed
7.582 km/s
True Right ascension
23h 25m 16s
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
08:58:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
557.81 km
Perigee altitude
549.535 km
Semi-major axis
6,931.81 km
Eccentricity
0.0006
Inclination
98.0845°
RAAN
351.3193°
Arg. of periapsis
278.8338°
True anomaly
81.28861°
Mean anomaly
81.221°
Eccentric anomaly
81.2548°
Mean motion
3.76074 °/min
Orbital period
95.73 mins
BSTAR
0.00030072
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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 | 2026-01-05 11:31:11.102Z | 25.547° NE | 2026-01-05 11:34:11.102Z | 79.17° E | 36.99° | 2026-01-05 11:38:11.102Z | 176.215° S |
| 5 mins | 2026-01-05 22:17:11.102Z | 118.938° SE | 2026-01-05 22:19:11.102Z | 77.202° E | 25.74° | 2026-01-05 22:22:11.102Z | 15.611° NNE |
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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