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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ICEYE-X6 radio frequencies
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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: 8 hours ago
TLE from 8 hours ago
0 ICEYE-X6
1 46497U 20068M 25261.91327730 .00004267 00000-0 33303-3 0 9998
2 46497 98.0728 238.4746 0003895 284.6863 75.3929 15.01711810272474Epoch: 2025-09-18T21:55Z
TLE epoch observation values (Epoch: 2025-09-18T21:55:07.158Z)
Latitude
0.00003°
Longitude
-88.37328°
Altitude
563.982 km
Speed
7.58 km/s
True Right ascension
15h 53m 53s
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
22:26:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
561.339 km
Perigee altitude
555.935 km
Semi-major axis
6,936.774 km
Eccentricity
0.00039
Inclination
98.0728°
RAAN
238.4746°
Arg. of periapsis
284.6863°
True anomaly
75.4361°
Mean anomaly
75.3929°
Eccentric anomaly
75.4145°
Mean motion
3.7567 °/min
Orbital period
95.83 mins
BSTAR
0.00033303
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-09-19 11:16:04.960Z | 17.879° NNE | 2025-09-19 11:20:04.960Z | 109.931° ESE | 42.998° | 2025-09-19 11:23:04.960Z | 183.771° SSW |
| 6 mins | 2025-09-19 22:03:04.960Z | 130.783° SE | 2025-09-19 22:05:04.960Z | 88.164° E | 31.119° | 2025-09-19 22:09:04.960Z | 4.237° 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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