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 25292.95791941 .00011212 00000-0 85293-3 0 9998
2 46497 98.0773 270.7744 0007260 164.5254 195.6193 15.02281147277134Epoch: 2025-10-19T22:59Z
TLE epoch observation values (Epoch: 2025-10-19T22:59:24.237Z)
Latitude
0.00002°
Longitude
-102.74371°
Altitude
567.763 km
Speed
7.575 km/s
True Right ascension
18h 03m 05s
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
22:38:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
561.918 km
Perigee altitude
551.849 km
Semi-major axis
6,935.02 km
Eccentricity
0.00073
Inclination
98.0773°
RAAN
270.7744°
Arg. of periapsis
164.5254°
True anomaly
195.59692°
Mean anomaly
195.6193°
Eccentric anomaly
195.60811°
Mean motion
3.75813 °/min
Orbital period
95.79 mins
BSTAR
0.00085293
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-20 10:46:02.991Z | 51.311° ENE | 2025-10-20 10:48:02.991Z | 88.223° E | 21.223° | 2025-10-20 10:51:02.991Z | 144.673° SSE |
| 5 mins | 2025-10-20 12:21:02.991Z | 333.801° NNW | 2025-10-20 12:23:02.991Z | 293.912° NW | 22.391° | 2025-10-20 12:26:02.991Z | 239.361° WSW |
| 6 mins | 2025-10-20 23:06:02.991Z | 198.15° SSW | 2025-10-20 23:09:02.991Z | 280.549° WNW | 32.371° | 2025-10-20 23:12:02.991Z | 330.678° 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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