Showing default

COSMOS 2426 (GLONASS), 29671

Orbit data source: Space-Track

COSMOS 2426 (GLONASS), 29671 is a Commonwealth of Independent States-origin payload satellite in MEO that was launched on Mon, 25 Dec 2006 UTC via a PROTON-K/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
29671, 2006-062B
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)
2006-12-25 (19 years ago)
Launch vehicle
PROTON-K/DM-2
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Arm + 2 Pan, 3.9 m
Radar Cross Section
8.145 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 5 days ago

TLE from 5 days ago
0 COSMOS 2426 (GLONASS)
1 29671U 06062B   25344.57884740  .00000044  00000-0  00000+0 0  9997
2 29671  64.6969 200.8040 0021659 178.5174 352.3152  2.12963481147534
Epoch: 2025-12-10T13:53Z
TLE epoch observation values (Epoch: 2025-12-10T13:53:32.415Z)
Latitude
8.33518°
Longitude
88.90786°
Altitude
19,086.082 km
Speed
3.961 km/s
True Right ascension
01h 07m 21s
True Declination
8° 19' 17"
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
00:00:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,195.844 km
Perigee altitude
19,085.302 km
Semi-major axis
25,518.71 km
Eccentricity
0.00217
Inclination
64.6969°
RAAN
200.804°
Arg. of periapsis
178.5174°
True anomaly
352.28192°
Mean anomaly
352.3152°
Eccentric anomaly
352.29857°
Mean motion
0.53242 °/min
Orbital period
676.16 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
|