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: 3 hours ago
TLE from 3 hours ago
0 ICEYE-X7
1 46496U 20068L 26305.23331603 .00009107 00000-0 27936-3 0 9999
2 46496 97.7673 278.3811 0006365 185.9353 174.1814 15.33987173335783Epoch: 2026-11-01T05:35Z
TLE epoch observation values (Epoch: 2026-11-01T05:35:58.504Z)
Latitude
-0.00009°
Longitude
153.85972°
Altitude
471.363 km
Speed
7.628 km/s
True Right ascension
18h 33m 31s
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
04:41:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
465.247 km
Perigee altitude
456.541 km
Semi-major axis
6,839.031 km
Eccentricity
0.00064
Inclination
97.7673°
RAAN
278.3811°
Arg. of periapsis
185.9353°
True anomaly
174.18879°
Mean anomaly
174.1814°
Eccentric anomaly
174.18509°
Mean motion
3.83753 °/min
Orbital period
93.81 mins
BSTAR
0.00027936
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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 | 2026-11-01 10:51:14.076Z | 28.253° NE | 2026-11-01 10:54:14.076Z | 88.969° E | 39.312° | 2026-11-01 10:57:14.076Z | 167.321° S |
| 4 mins | 2026-11-01 22:58:14.076Z | 226.292° WSW | 2026-11-01 22:59:14.076Z | 255.748° W | 29.359° | 2026-11-01 23:02:14.076Z | 322.669° NNW |
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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