Showing default

COSMOS 2425 (GLONASS), 29670

Orbit data source: Space-Track

COSMOS 2425 (GLONASS), 29670 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
29670, 2006-062A
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: 2 days ago

TLE from 2 days ago
0 COSMOS 2425 (GLONASS)
1 29670U 06062A   26077.47544577  .00000021  00000-0  00000-0 0  9996
2 29670  64.6927 197.2997 0022397 356.6901   0.0474  2.13117176149645
Epoch: 2026-03-18T11:24Z
TLE epoch observation values (Epoch: 2026-03-18T11:24:38.514Z)
Latitude
-2.93858°
Longitude
-151.29074°
Altitude
19,072.543 km
Speed
3.962 km/s
True Right ascension
13h 03m 38s
True Declination
-2° 56' 01"
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
23:32:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,185.429 km
Perigee altitude
19,071.175 km
Semi-major axis
25,506.439 km
Eccentricity
0.00224
Inclination
64.6927°
RAAN
197.2997°
Arg. of periapsis
356.6901°
True anomaly
0.04761°
Mean anomaly
0.0474°
Eccentric anomaly
0.04751°
Mean motion
0.53281 °/min
Orbital period
675.67 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
|