Showing default

GONETS M 15 (M25), 44906

Orbit data source: Space-Track

GONETS M 15 (M25), 44906 is a payload satellite owned by Gonets (CIS) in LEO that was launched on Thu, 26 Dec 2019 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
44906, 2019-096B
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)
2019-12-26 (6 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: 14 hours ago

TLE from 14 hours ago
0 GONETS M 15 (M25)
1 44906U 19096B   25311.30458693  .00000047  00000-0  26530-3 0  9998
2 44906  82.5275 222.5851 0015199 304.4319  55.5324 12.42863793266089
Epoch: 2025-11-07T07:18Z
TLE epoch observation values (Epoch: 2025-11-07T07:18:36.310Z)
Latitude
-0°
Longitude
66.18334°
Altitude
1,490.426 km
Speed
7.122 km/s
True Right ascension
14h 50m 20s
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
17:41:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,503.798 km
Perigee altitude
1,479.875 km
Semi-major axis
7,869.974 km
Eccentricity
0.00152
Inclination
82.5275°
RAAN
222.5851°
Arg. of periapsis
304.4319°
True anomaly
55.67615°
Mean anomaly
55.5324°
Eccentric anomaly
55.60426°
Mean motion
3.10873 °/min
Orbital period
115.8 mins
BSTAR
0.0002653
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...
Other satellites on launch #96 in the year 2019 (2019-12-26 UTC)

Documentation

Showing up to 5 results
|