Showing default

GONETS M 17, 46486

Orbit data source: Space-Track

GONETS M 17, 46486 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
46486, 2020-068A
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: 15 hours ago

TLE from 15 hours ago
0 GONETS M 17
1 46486U 20068A   26127.23594868 -.00000020  00000-0 -21445-3 0  9990
2 46486  82.5019  12.9793 0023083 122.5940 237.7373 12.42871443254071
Epoch: 2026-05-07T05:39Z
TLE epoch observation values (Epoch: 2026-05-07T05:39:45.965Z)
Latitude
0.00002°
Longitude
62.95279°
Altitude
1,506.886 km
Speed
7.107 km/s
True Right ascension
00h 51m 55s
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
04:40:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,509.972 km
Perigee altitude
1,473.639 km
Semi-major axis
7,869.942 km
Eccentricity
0.00231
Inclination
82.5019°
RAAN
12.9793°
Arg. of periapsis
122.594°
True anomaly
237.51397°
Mean anomaly
237.7373°
Eccentric anomaly
237.6256°
Mean motion
3.10875 °/min
Orbital period
115.8 mins
BSTAR
-0.00021445
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|