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: 1 day ago
TLE from 1 day ago
0 ICEYE-X6
1 46497U 20068M 25306.54461241 .00008550 00000-0 64742-3 0 9993
2 46497 98.0812 284.9308 0009226 119.5538 240.6607 15.02526678279178Epoch: 2025-11-02T13:04Z
TLE epoch observation values (Epoch: 2025-11-02T13:04:14.512Z)
Latitude
0.00005°
Longitude
46.81151°
Altitude
565.296 km
Speed
7.577 km/s
True Right ascension
18h 59m 43s
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
15:46:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.525 km
Perigee altitude
549.73 km
Semi-major axis
6,934.264 km
Eccentricity
0.00092
Inclination
98.0812°
RAAN
284.9308°
Arg. of periapsis
119.5538°
True anomaly
240.56859°
Mean anomaly
240.6607°
Eccentric anomaly
240.61464°
Mean motion
3.75874 °/min
Orbital period
95.78 mins
BSTAR
0.00064742
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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 | 2025-11-03 22:44:54.525Z | 169.315° S | 2025-11-03 22:48:54.525Z | 294.311° NW | 44.487° | 2025-11-03 22:51:54.525Z | 344.408° N |
| 5 mins | 2025-11-04 11:59:54.525Z | 349.713° N | 2025-11-04 12:01:54.525Z | 295.107° NW | 35.805° | 2025-11-04 12:04:54.525Z | 218.398° SW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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