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: 15 hours ago
TLE from 15 hours ago
0 ICEYE-X6
1 46497U 20068M 26274.25362968 .00000750 00000-0 57735-4 0 9991
2 46497 98.1059 273.0780 0008843 93.3882 266.8354 15.04961613329180Epoch: 2026-10-01T06:05Z
TLE epoch observation values (Epoch: 2026-10-01T06:05:13.604Z)
Latitude
-0.00007°
Longitude
171.77875°
Altitude
555.016 km
Speed
7.584 km/s
True Right ascension
18h 12m 18s
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
14:51:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
554.766 km
Perigee altitude
542.515 km
Semi-major axis
6,926.778 km
Eccentricity
0.00088
Inclination
98.1059°
RAAN
273.078°
Arg. of periapsis
93.3882°
True anomaly
266.73423°
Mean anomaly
266.8354°
Eccentric anomaly
266.78481°
Mean motion
3.76484 °/min
Orbital period
95.62 mins
BSTAR
0.000057735
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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 | 2026-10-01 23:46:05.888Z | 149.409° SSE | 2026-10-01 23:49:05.888Z | 87.431° E | 54.611° | 2026-10-01 23:53:05.888Z | 356.438° N |
| 6 mins | 2026-10-02 12:59:05.888Z | 11.922° NNE | 2026-10-02 13:01:05.888Z | 3.786° NNE | 75.846° | 2026-10-02 13:05:05.888Z | 194.895° SSW |
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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