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: 9 hours ago
TLE from 9 hours ago
0 ICEYE-X6
1 46497U 20068M 26263.21650407 .00001985 00000-0 14492-3 0 9996
2 46497 98.1050 261.4965 0008152 125.1066 235.0925 15.04926760327520Epoch: 2026-09-20T05:11Z
TLE epoch observation values (Epoch: 2026-09-20T05:11:45.951Z)
Latitude
0.00005°
Longitude
-175.55884°
Altitude
558.016 km
Speed
7.581 km/s
True Right ascension
17h 25m 59s
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
06:46:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
554.394 km
Perigee altitude
543.101 km
Semi-major axis
6,926.885 km
Eccentricity
0.00082
Inclination
98.105°
RAAN
261.4965°
Arg. of periapsis
125.1066°
True anomaly
235.01594°
Mean anomaly
235.0925°
Eccentric anomaly
235.05421°
Mean motion
3.76475 °/min
Orbital period
95.62 mins
BSTAR
0.00014492
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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 | 2026-09-21 00:28:25.006Z | 197.923° SSW | 2026-09-21 00:31:25.006Z | 273.024° WNW | 38.478° | 2026-09-21 00:34:25.006Z | 328.738° NNW |
| 5 mins | 2026-09-21 12:06:25.006Z | 56.069° ENE | 2026-09-21 12:08:25.006Z | 95.482° ESE | 22.151° | 2026-09-21 12:11:25.006Z | 147.003° SSE |
| 4 mins | 2026-09-21 13:41:25.006Z | 327.525° NNW | 2026-09-21 13:43:25.006Z | 281.937° WNW | 24.692° | 2026-09-21 13:45:25.006Z | 244.151° WSW |
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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