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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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: 9 hours ago
TLE from 9 hours ago
0 ICEYE-X6
1 46497U 20068M 25275.90487503 .00012233 00000-0 93733-3 0 9992
2 46497 98.0715 253.0263 0005579 223.3912 136.6873 15.01988967274574Epoch: 2025-10-02T21:43Z
TLE epoch observation values (Epoch: 2025-10-02T21:43:01.202Z)
Latitude
-0.00001°
Longitude
-84.58754°
Altitude
566.628 km
Speed
7.576 km/s
True Right ascension
16h 52m 06s
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
00:15:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
561.653 km
Perigee altitude
553.914 km
Semi-major axis
6,935.92 km
Eccentricity
0.00056
Inclination
98.0715°
RAAN
253.0263°
Arg. of periapsis
223.3912°
True anomaly
136.73113°
Mean anomaly
136.6873°
Eccentric anomaly
136.70922°
Mean motion
3.7574 °/min
Orbital period
95.81 mins
BSTAR
0.00093733
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-03 11:05:00.363Z | 31.675° NE | 2025-10-03 11:08:00.363Z | 103.503° ESE | 34.599° | 2025-10-03 11:11:00.363Z | 168.523° S |
| 4 mins | 2025-10-03 21:52:00.363Z | 101.915° ESE | 2025-10-03 21:53:00.363Z | 79.657° E | 23.38° | 2025-10-03 21:56:00.363Z | 19.429° NNE |
| 4 mins | 2025-10-03 23:27:00.363Z | 238.123° WSW | 2025-10-03 23:28:00.363Z | 259.085° W | 20.594° | 2025-10-03 23:31:00.363Z | 312.826° NW |
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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