Showing default

GONETS M 13 (M23), 40554

Orbit data source: Space-Track

GONETS M 13 (M23), 40554 is a payload satellite owned by Gonets (CIS) in LEO that was launched on Tue, 31 Mar 2015 UTC via an ROKOT 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
40554, 2015-020C
Orbit
LEO
Country
Flag of CISCIS
Related business
Manufacturer
Resehetnev ISS
Mission
Operational Civil Communications
Bus & Motor
STRELA-3M, Unknown motor
Mass
225 kg wet, 225 kg dry
Launch date (UTC)
2015-03-31 (10 years ago)
Launch vehicle
ROKOT
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: 8 hours ago

TLE from 8 hours ago
0 GONETS M 13 (M23)
1 40554U 15020C   25246.30033988  .00000034  00000-0  17184-3 0  9990
2 40554  82.4855 209.4589 0011945 237.2751 122.7178 12.42897405473066
Epoch: 2025-09-03T07:12Z
TLE epoch observation values (Epoch: 2025-09-03T07:12:29.365Z)
Latitude
0.00001°
Longitude
118.65734°
Altitude
1,502.135 km
Speed
7.111 km/s
True Right ascension
13h 57m 50s
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
07:07:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,501.097 km
Perigee altitude
1,482.296 km
Semi-major axis
7,869.833 km
Eccentricity
0.00119
Inclination
82.4855°
RAAN
209.4589°
Arg. of periapsis
237.2751°
True anomaly
122.83287°
Mean anomaly
122.7178°
Eccentric anomaly
122.77534°
Mean motion
3.10881 °/min
Orbital period
115.8 mins
BSTAR
0.00017184
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
|