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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). Payloads include a variety of satellites, spacecraft, and rockets 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.

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COSMOS 2425 (GLONASS) details

Identifier	29670, 2006-062A
Orbit	MEO
Last TLE update	2 days ago
Origin	KVR/IACG (CIS)
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 (18 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, 7.8 m
Radar Cross Section	8.145 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 2 days ago

0 COSMOS 2425 (GLONASS)
1 29670U 06062A   24359.20049344  .00000085  00000-0  00000-0 0  9990
2 29670  64.6908 212.2664 0021775 358.8307 185.5504  2.13117865140072

Epoch: 2024-12-24T04:48Z

Definitive object data (Epoch: 2024-12-24T04:48:42.633Z)

Latitude	-3.93156°
Longitude	-131.25829°
Altitude	19,185.09 km
Speed	3.945 km/s
True Right ascension	02h 16m 31s
True Declination	-3° 55' 30"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	64.23824°
Longitude	148.6118°
Altitude	19,144.937 km
Speed	3.953 km/s
Apparent Right ascension	21h 09m 33s
Apparent Declination	49° 51' 09"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	09:40:21
Azimuth	4.956° NNE
Elevation	0.024°
Doppler factor	1

Orbital elements

Apogee altitude	19,183.787 km
Perigee altitude	19,072.707 km
Semi-major axis	25,506.384 km
Eccentricity	0.0021775
Inclination	64.6908°
RAAN	212.2664°
Arg. of periapsis	358.8307°
True anomaly	185.52633°
Mean anomaly	185.5504°
Eccentric anomaly	185.53836°
Mean motion	0.53281 °/min
BSTAR	Unknown
Orbital period	675.67 mins