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 (6 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 19
1 46488U 20068C   26124.59973747  .00000193  00000-0  13186-2 0  9996
2 46488  82.5006  14.1958 0013817 137.7403 222.4744 12.42891335253830
Epoch: 2026-05-04T14:23Z
TLE epoch observation values (Epoch: 2026-05-04T14:23:37.317Z)
Latitude
-0.00001°
Longitude
-64.1963°
Altitude
1,505.101 km
Speed
7.108 km/s
True Right ascension
00h 56m 46s
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
05:03:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,502.595 km
Perigee altitude
1,480.848 km
Semi-major axis
7,869.858 km
Eccentricity
0.00138
Inclination
82.5006°
RAAN
14.1958°
Arg. of periapsis
137.7403°
True anomaly
222.36762°
Mean anomaly
222.4744°
Eccentric anomaly
222.421°
Mean motion
3.1088 °/min
Orbital period
115.8 mins
BSTAR
0.0013186
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
|