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: 6 hours ago
TLE from 6 hours ago
0 ICEYE-X6
1 46497U 20068M 26183.62064981 .00002886 00000-0 21026-3 0 9990
2 46497 98.0967 178.0309 0008271 47.8303 312.3623 15.04602961315555Epoch: 2026-07-02T14:53Z
TLE epoch observation values (Epoch: 2026-07-02T14:53:44.143Z)
Latitude
-0.00002°
Longitude
33.93655°
Altitude
551.913 km
Speed
7.588 km/s
True Right ascension
11h 52m 07s
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
08:35:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
555.472 km
Perigee altitude
544.012 km
Semi-major axis
6,927.879 km
Eccentricity
0.00083
Inclination
98.0967°
RAAN
178.0309°
Arg. of periapsis
47.8303°
True anomaly
312.29222°
Mean anomaly
312.3623°
Eccentric anomaly
312.32726°
Mean motion
3.76394 °/min
Orbital period
95.64 mins
BSTAR
0.00021026
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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 | 2026-07-02 23:00:51.123Z | 127.714° SE | 2026-07-02 23:03:51.123Z | 69.523° E | 26.129° | 2026-07-02 23:06:51.123Z | 12.488° NNE |
| 4 mins | 2026-07-03 00:36:51.123Z | 233.318° WSW | 2026-07-03 00:38:51.123Z | 270.971° WNW | 17.53° | 2026-07-03 00:40:51.123Z | 304.982° NW |
| 5 mins | 2026-07-03 12:13:51.123Z | 36.448° NE | 2026-07-03 12:15:51.123Z | 93.785° ESE | 36.302° | 2026-07-03 12:18:51.123Z | 170.244° S |
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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