Showing default

GONETS M 18, 46487

Orbit data source: Space-Track

GONETS M 18, 46487 is a payload satellite owned by Gonets (CIS) in LEO 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
46487, 2020-068B
Orbit
LEO
Country
Flag of CISCIS
Related business
Manufacturer
Resehetnev ISS
Mission
Operational Commercial Communications
Bus & Motor
STRELA-3M, Unknown motor
Mass
225 kg wet, 225 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
Cyl + 1 Ant, 3.5 m
Radar Cross Section
1.798 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 7 hours ago

TLE from 7 hours ago
0 GONETS M 18
1 46487U 20068B   25297.79865185  .00000033  00000-0  16386-3 0  9992
2 46487  82.4898 133.1574 0019820 184.2769 175.8144 12.42889667229906
Epoch: 2025-10-24T19:10Z
TLE epoch observation values (Epoch: 2025-10-24T19:10:03.519Z)
Latitude
-0.00007°
Longitude
172.20435°
Altitude
1,512.641 km
Speed
7.102 km/s
True Right ascension
08h 52m 37s
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
21:20:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,507.327 km
Perigee altitude
1,476.131 km
Semi-major axis
7,869.866 km
Eccentricity
0.00198
Inclination
82.4898°
RAAN
133.1574°
Arg. of periapsis
184.2769°
True anomaly
175.83094°
Mean anomaly
175.8144°
Eccentric anomaly
175.82267°
Mean motion
3.1088 °/min
Orbital period
115.8 mins
BSTAR
0.00016386
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
|