Showing default

COSMOS 2475 (GLONASS), 37869

Orbit data source: Space-Track

COSMOS 2475 (GLONASS), 37869 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
37869, 2011-064C
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 (14 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: 19 hours ago

TLE from 19 hours ago
0 COSMOS 2475 (GLONASS)
1 37869U 11064C   25349.78732626 -.00000056  00000-0  00000-0 0  9991
2 37869  65.1780  79.1657 0026329 248.6854 113.9368  2.13101578109869
Epoch: 2025-12-15T18:53Z
TLE epoch observation values (Epoch: 2025-12-15T18:53:44.988Z)
Latitude
2.62165°
Longitude
72.26336°
Altitude
19,157.67 km
Speed
3.949 km/s
True Right ascension
05h 21m 31s
True Declination
2° 37' 02"
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
12:11:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,196.689 km
Perigee altitude
19,062.371 km
Semi-major axis
25,507.667 km
Eccentricity
0.00263
Inclination
65.178°
RAAN
79.1657°
Arg. of periapsis
248.6854°
True anomaly
114.21219°
Mean anomaly
113.9368°
Eccentric anomaly
114.07453°
Mean motion
0.53277 °/min
Orbital period
675.72 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
|