Showing default

METEOR 2-5, 11605

Orbit data source: Space-Track

METEOR 2-5, 11605 is a Commonwealth of Independent States-origin payload satellite in LEO that was launched on Wed, 31 Oct 1979 UTC via a VOSTOK 8A92M 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
11605, 1979-095A
Orbit
LEO
Country
Flag of CISCIS
Related business
Manufacturer
VNIIEM
Mission
Spacecraft
Bus & Motor
METEOR-2, Unknown motor
Mass
~1,500 kg wet, ~1,500 kg dry
Launch date (UTC)
1979-10-31 (46 years ago)
Launch vehicle
VOSTOK 8A92M
Launch site
Plesetsk Missile And Space Complex (PKMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 METEOR 2-5
1 11605U 79095A   25308.48205765  .00000041  00000-0  16838-4 0  9993
2 11605  81.2078  90.0033 0008899 163.4123 196.7339 14.07434231361692
Epoch: 2025-11-04T11:34Z
TLE epoch observation values (Epoch: 2025-11-04T11:34:09.780Z)
Latitude
-0.00006°
Longitude
-127.50591°
Altitude
877.237 km
Speed
7.411 km/s
True Right ascension
06h 00m 00s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
16:51:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
871.79 km
Perigee altitude
858.898 km
Semi-major axis
7,243.481 km
Eccentricity
0.00089
Inclination
81.2078°
RAAN
90.0033°
Arg. of periapsis
163.4123°
True anomaly
196.70457°
Mean anomaly
196.7339°
Eccentric anomaly
196.71923°
Mean motion
3.52064 °/min
Orbital period
102.25 mins
BSTAR
0.000016838
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|