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 26126.95343274 .00001937 00000-0 14388-3 0 9997
2 46497 98.0975 118.6658 0005917 216.5179 143.5643 15.04307222307033Epoch: 2026-05-06T22:52Z
TLE epoch observation values (Epoch: 2026-05-06T22:52:56.588Z)
Latitude
-0.00002°
Longitude
-89.37651°
Altitude
559.983 km
Speed
7.58 km/s
True Right ascension
07h 54m 39s
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
12:24:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
554.75 km
Perigee altitude
546.551 km
Semi-major axis
6,928.788 km
Eccentricity
0.00059
Inclination
98.0975°
RAAN
118.6658°
Arg. of periapsis
216.5179°
True anomaly
143.60455°
Mean anomaly
143.5643°
Eccentric anomaly
143.58443°
Mean motion
3.7632 °/min
Orbital period
95.66 mins
BSTAR
0.00014388
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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 | 2026-05-07 12:13:23.767Z | 18.165° NNE | 2026-05-07 12:16:23.767Z | 95.838° ESE | 43.863° | 2026-05-07 12:19:23.767Z | 186.242° SSW |
| 6 mins | 2026-05-07 22:58:23.767Z | 132.361° SE | 2026-05-07 23:00:23.767Z | 89.278° E | 31.852° | 2026-05-07 23:04:23.767Z | 3.414° NNE |
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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