Showing default

COSMOS 2500 (GLONASS), 40001

Orbit data source: Space-Track

COSMOS 2500 (GLONASS), 40001 is a Commonwealth of Independent States-origin payload satellite in MEO that was launched on Sat, 14 Jun 2014 UTC via a SOYUZ-2-1B launch vehicle from the Plesetsk Missile And Space Complex (PKMTR). 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
40001, 2014-032A
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)
2014-06-14 (11 years ago)
Launch vehicle
SOYUZ-2-1B
Launch site
Plesetsk Missile And Space Complex (PKMTR)
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: 9 hours ago

TLE from 9 hours ago
0 COSMOS 2500 (GLONASS)
1 40001U 14032A   25343.46028346 -.00000049  00000-0  00000-0 0  9999
2 40001  65.3451 320.1442 0008310 219.1348 140.8020  2.13105796 89418
Epoch: 2025-12-09T11:02Z
TLE epoch observation values (Epoch: 2025-12-09T11:02:48.490Z)
Latitude
-0.00004°
Longitude
75.98579°
Altitude
19,146.565 km
Speed
3.951 km/s
True Right ascension
21h 20m 31s
True Declination
0° 00' 00"
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
18:21:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,150.384 km
Perigee altitude
19,107.991 km
Semi-major axis
25,507.325 km
Eccentricity
0.00083
Inclination
65.3451°
RAAN
320.1442°
Arg. of periapsis
219.1348°
True anomaly
140.86213°
Mean anomaly
140.802°
Eccentric anomaly
140.83207°
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...
Other satellites on launch #32 in the year 2014 (2014-06-14 UTC)

Documentation

Showing up to 5 results
|