ICEYE-X7, 46496
Orbit data source: Space-Track
ICEYE-X7, 46496 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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46496 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: 4 hours ago
TLE from 4 hours ago
0 ICEYE-X7
1 46496U 20068L 26252.31518809 .00008689 00000-0 27412-3 0 9997
2 46496 97.7575 222.8050 0008573 42.1222 318.0676 15.33093362327677Epoch: 2026-09-09T07:33Z
TLE epoch observation values (Epoch: 2026-09-09T07:33:52.250Z)
Latitude
-0.00012°
Longitude
120.96829°
Altitude
465.323 km
Speed
7.636 km/s
True Right ascension
14h 51m 13s
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
04:15:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
469.419 km
Perigee altitude
457.688 km
Semi-major axis
6,841.69 km
Eccentricity
0.00086
Inclination
97.7575°
RAAN
222.805°
Arg. of periapsis
42.1222°
True anomaly
318.0019°
Mean anomaly
318.0676°
Eccentric anomaly
318.03475°
Mean motion
3.83529 °/min
Orbital period
93.87 mins
BSTAR
0.00027412
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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-X7 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 | 2026-09-09 21:47:33.216Z | 143.679° SSE | 2026-09-09 21:50:33.216Z | 70.689° E | 42.461° | 2026-09-09 21:53:33.216Z | 2.948° NNE |
| 5 mins | 2026-09-10 10:46:33.216Z | 35.598° NE | 2026-09-10 10:48:33.216Z | 122.593° SE | 49.107° | 2026-09-10 10:51:33.216Z | 177.495° S |
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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