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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Edit Public Description
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, 1.6 m
Radar Cross Section
1.837 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 ICEYE-X7
1 46496U 20068L 26020.30807711 .00032753 00000-0 12135-2 0 9996
2 46496 97.7343 340.6939 0010157 119.7010 240.5241 15.27526458292186Epoch: 2026-01-20T07:23Z
TLE epoch observation values (Epoch: 2026-01-20T07:23:37.862Z)
Latitude
0.00003°
Longitude
110.09432°
Altitude
489.736 km
Speed
7.618 km/s
True Right ascension
22h 42m 46s
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
20:55:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
487.146 km
Perigee altitude
473.214 km
Semi-major axis
6,858.317 km
Eccentricity
0.00102
Inclination
97.7343°
RAAN
340.6939°
Arg. of periapsis
119.701°
True anomaly
240.42284°
Mean anomaly
240.5241°
Eccentric anomaly
240.47346°
Mean motion
3.82135 °/min
Orbital period
94.21 mins
BSTAR
0.0012135
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-01-20 21:41:26.910Z | 210.155° SW | 2026-01-20 21:42:26.910Z | 240.095° WSW | 31.46° | 2026-01-20 21:45:26.910Z | 326.294° NNW |
| 4 mins | 2026-01-21 10:41:26.910Z | 337.544° N | 2026-01-21 10:43:26.910Z | 282.308° WNW | 27.218° | 2026-01-21 10:45:26.910Z | 234.238° WSW |
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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