Showing default

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.

Loading next visibility...
Identifier
46497, 2020-068M
Orbit
SSO
Country
Flag of FIFI / FIN
Related business
Manufacturer
ICEYE
Mission
Operational Commercial Radar Imaging
Bus & Motor
ICEYE, Unknown motor
Mass
80 kg wet, 80 kg dry
Launch date (UTC)
2020-09-28 (5 years ago)
Launch vehicle
SOYUZ-2-1B
Launch site
Plesetsk Missile And Space Complex (PKMTR)
Object type
Payload
Rocket body
Debris
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 & history
Last TLE update: 10 hours ago

TLE from 10 hours ago
0 ICEYE-X6
1 46497U 20068M   25261.24695773  .00003809  00000-0  29789-3 0  9993
2 46497  98.0729 237.7816 0003845 288.2487  71.8317 15.01705361272377
Epoch: 2025-09-18T05:55Z
TLE epoch observation values (Epoch: 2025-09-18T05:55:37.147Z)
Latitude
-0.00011°
Longitude
151.46554°
Altitude
563.852 km
Speed
7.58 km/s
True Right ascension
15h 51m 07s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
08:22:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
561.324 km
Perigee altitude
555.99 km
Semi-major axis
6,936.794 km
Eccentricity
0.00038
Inclination
98.0729°
RAAN
237.7816°
Arg. of periapsis
288.2487°
True anomaly
71.87357°
Mean anomaly
71.8317°
Eccentric anomaly
71.85263°
Mean motion
3.75669 °/min
Orbital period
95.83 mins
BSTAR
0.00029789
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|