Showing default

COSMOS 2447 (GLONASS), 33466

Orbit data source: Space-Track

COSMOS 2447 (GLONASS), 33466 is a Commonwealth of Independent States-origin payload satellite in MEO that was launched on Thu, 25 Dec 2008 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
33466, 2008-067A
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)
2008-12-25 (17 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: 1 day ago

TLE from 1 day ago
0 COSMOS 2447 (GLONASS)
1 33466U 08067A   26125.33169723 -.00000010  00000-0  00000-0 0  9995
2 33466  64.7957  70.8222 0008307 268.8559 270.8815  2.13108092135055
Epoch: 2026-05-05T07:57Z
TLE epoch observation values (Epoch: 2026-05-05T07:57:38.640Z)
Latitude
0.25169°
Longitude
-91.92292°
Altitude
19,129.599 km
Speed
3.953 km/s
True Right ascension
16h 42m 47s
True Declination
0° 15' 05"
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
19:12:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,150.212 km
Perigee altitude
19,107.835 km
Semi-major axis
25,507.16 km
Eccentricity
0.00083
Inclination
64.7957°
RAAN
70.8222°
Arg. of periapsis
268.8559°
True anomaly
270.78632°
Mean anomaly
270.8815°
Eccentric anomaly
270.83391°
Mean motion
0.53278 °/min
Orbital period
675.7 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
|