Showing default

COSMOS 2466 (GLONASS), 37137

Orbit data source: Space-Track

COSMOS 2466 (GLONASS), 37137 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
37137, 2010-041A
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 (16 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 days ago

TLE from 2 days ago
0 COSMOS 2466 (GLONASS)
1 37137U 10041A   26205.87641693  .00000076  00000-0  00000-0 0  9999
2 37137  63.8967 188.7878 0017101 178.6795  31.0570  2.13111911123644
Epoch: 2026-07-24T21:02Z
TLE epoch observation values (Epoch: 2026-07-24T21:02:02.422Z)
Latitude
-26.61978°
Longitude
124.88755°
Altitude
19,099.778 km
Speed
3.958 km/s
True Right ascension
01h 31m 58s
True Declination
-26° 34' 53"
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
22:23:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,172.37 km
Perigee altitude
19,085.131 km
Semi-major axis
25,506.887 km
Eccentricity
0.00171
Inclination
63.8967°
RAAN
188.7878°
Arg. of periapsis
178.6795°
True anomaly
31.15828°
Mean anomaly
31.057°
Eccentric anomaly
31.10762°
Mean motion
0.53279 °/min
Orbital period
675.69 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
|