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: 4 hours ago
TLE from 4 hours ago
0 ICEYE-X7
1 46496U 20068L 25288.98595652 .00014136 00000-0 57710-3 0 9997
2 46496 97.7188 241.1453 0011433 101.2550 258.9972 15.24463354277495Epoch: 2025-10-15T23:39Z
TLE epoch observation values (Epoch: 2025-10-15T23:39:46.643Z)
Latitude
-0.00003°
Longitude
-138.55121°
Altitude
496.993 km
Speed
7.615 km/s
True Right ascension
16h 04m 34s
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
22:25:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
497.223 km
Perigee altitude
481.519 km
Semi-major axis
6,867.508 km
Eccentricity
0.00114
Inclination
97.7188°
RAAN
241.1453°
Arg. of periapsis
101.255°
True anomaly
258.86863°
Mean anomaly
258.9972°
Eccentric anomaly
258.93291°
Mean motion
3.81368 °/min
Orbital period
94.4 mins
BSTAR
0.0005771
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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 | 2025-10-16 09:40:24.178Z | 18.46° NNE | 2025-10-16 09:43:24.178Z | 81.024° E | 42.602° | 2025-10-16 09:46:24.178Z | 183.651° SSW |
| 4 mins | 2025-10-16 20:18:24.178Z | 102.982° ESE | 2025-10-16 20:19:24.178Z | 77.685° E | 23.028° | 2025-10-16 20:22:24.178Z | 15.995° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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