Showing default

COSMOS 2477 (GLONASS), 37868

Orbit data source: Space-Track

COSMOS 2477 (GLONASS), 37868 is a Commonwealth of Independent States-origin payload satellite in MEO that was launched on Fri, 04 Nov 2011 UTC via a PROTON-M/BRIZ-M 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
37868, 2011-064B
Orbit
MEO
Country
Flag of CISCIS
Related business
Manufacturer
Resehetnev ISS
Mission
Operational Defense Navigation
Bus & Motor
URAGAN, Unknown motor
Mass
1,450 kg wet, ~1,200 kg dry
Launch date (UTC)
2011-11-04 (15 years ago)
Launch vehicle
PROTON-M/BRIZ-M
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: 16 hours ago

TLE from 16 hours ago
0 COSMOS 2477 (GLONASS)
1 37868U 11064B   26255.72261178 -.00000004  00000-0  00000-0 0  9993
2 37868  65.3306  69.9989 0019372 230.6947 308.5255  2.13102613115622
Epoch: 2026-09-12T17:20Z
TLE epoch observation values (Epoch: 2026-09-12T17:20:33.657Z)
Latitude
0.8405°
Longitude
-2.26701°
Altitude
19,099.653 km
Speed
3.958 km/s
True Right ascension
16h 38m 24s
True Declination
0° 50' 21"
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
02:03:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,178.855 km
Perigee altitude
19,080.029 km
Semi-major axis
25,507.579 km
Eccentricity
0.00194
Inclination
65.3306°
RAAN
69.9989°
Arg. of periapsis
230.6947°
True anomaly
308.35157°
Mean anomaly
308.5255°
Eccentric anomaly
308.43856°
Mean motion
0.53277 °/min
Orbital period
675.71 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
|