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 Commercial Communications
Bus & Motor
STRELA-3M, Unknown motor
Mass
225 kg wet, 225 kg dry
Launch date (UTC)
2015-03-31 (11 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   25331.95094299  .00000038  00000-0  20304-3 0  9990
2 40554  82.4834 156.1231 0013971  52.3101 307.9243 12.42862529483702
Epoch: 2025-11-27T22:49Z
TLE epoch observation values (Epoch: 2025-11-27T22:49:21.474Z)
Latitude
-0.00004°
Longitude
106.68313°
Altitude
1,490.439 km
Speed
7.122 km/s
True Right ascension
10h 24m 29s
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
04:32:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,502.839 km
Perigee altitude
1,480.849 km
Semi-major axis
7,869.981 km
Eccentricity
0.0014
Inclination
82.4834°
RAAN
156.1231°
Arg. of periapsis
52.3101°
True anomaly
307.79788°
Mean anomaly
307.9243°
Eccentric anomaly
307.8611°
Mean motion
3.10873 °/min
Orbital period
115.8 mins
BSTAR
0.00020304
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
|