Showing default

GONETS M 19, 46488

Orbit data source: Space-Track

GONETS M 19, 46488 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
46488, 2020-068C
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: 13 hours ago

TLE from 13 hours ago
0 GONETS M 19
1 46488U 20068C   26020.27566909  .00000006  00000-0 -29955-4 0  9991
2 46488  82.4941  79.1235 0013509  15.0531 345.0948 12.42886161240873
Epoch: 2026-01-20T06:36Z
TLE epoch observation values (Epoch: 2026-01-20T06:36:57.809Z)
Latitude
-0.00003°
Longitude
-139.77725°
Altitude
1,486.814 km
Speed
7.125 km/s
True Right ascension
05h 16m 29s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
20:53:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,502.375 km
Perigee altitude
1,481.112 km
Semi-major axis
7,869.881 km
Eccentricity
0.00135
Inclination
82.4941°
RAAN
79.1235°
Arg. of periapsis
15.0531°
True anomaly
345.05492°
Mean anomaly
345.0948°
Eccentric anomaly
345.07486°
Mean motion
3.10879 °/min
Orbital period
115.8 mins
BSTAR
-0.000029955
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
|