Showing default

COSMOS 2465 (GLONASS), 37138

Orbit data source: Space-Track

COSMOS 2465 (GLONASS), 37138 is a Commonwealth of Independent States-origin payload satellite in MEO that was launched on Thu, 02 Sep 2010 UTC via a PROTON-M/DM-2 launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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
37138, 2010-041B
Orbit
MEO
Country
Flag of CISCIS
Related business
Manufacturer
Resehetnev ISS
Mission
Non-operational Defense Navigation
Bus & Motor
URAGAN, Unknown motor
Mass
1,450 kg wet, ~1,200 kg dry
Launch date (UTC)
2010-09-02 (15 years ago)
Launch vehicle
PROTON-M/DM-2
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Ant + 2 Pan, 3.9 m
Radar Cross Section
8.467 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 2 weeks ago

TLE from 2 weeks ago
0 COSMOS 2465 (GLONASS)
1 37138U 10041B   25276.07280440  .00000001  00000-0  00000-0 0  9996
2 37138  63.9081 199.0422 0040680 179.7706 304.8803  2.13098263117383
Epoch: 2025-10-03T01:44Z
TLE epoch observation values (Epoch: 2025-10-03T01:44:50.300Z)
Latitude
47.95485°
Longitude
-51.98667°
Altitude
19,077.334 km
Speed
3.963 km/s
True Right ascension
23h 04m 59s
True Declination
47° 54' 25"
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
10:06:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,233.605 km
Perigee altitude
19,026.073 km
Semi-major axis
25,507.976 km
Eccentricity
0.00407
Inclination
63.9081°
RAAN
199.0422°
Arg. of periapsis
179.7706°
True anomaly
304.49678°
Mean anomaly
304.8803°
Eccentric anomaly
304.68865°
Mean motion
0.53276 °/min
Orbital period
675.73 mins
BSTAR
0
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
|