METEOR 3-2

19336
Spacetrack Directory Number
1988-07-26
Orbit launches
1207.05 km
Average height
26107.87 km/h
Average velocity


Satellite information METEOR 3-2

Spacetrack Directory Name METEOR 3-2
Follow METEOR 3-2 METEOR 3-2 Tracker
Pass predictions METEOR 3-2 Pass predictions METEOR 3-2
Orbit launches 1988-07-26 (38 years ago)
Days in orbit 13936
Country/organisation of origin Commonwealth of Independent States (former USSR) (CIS)
Starting point PLMSC (Plesetsk Missile and Space Complex, Russia)
Perigee 1182 km
Apogee 1209 km
Orbit slope (inclination) 82.54°
Laps per day 13
Height METEOR 3-2 1207.05 km

Additional information METEOR 3-2

METEOR 3-2, 19336 is a payload satellite owned by GMS (CIS) in LEO that was launched on Tue, 26 Jul 1988 UTC via a TSIKLON-3 launch vehicle from the Plesetsk Missile And Space Complex (PKMTR). 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.

satellite METEOR 3-2 Date of exalting 26.07.1988y. Average height of ISS METEOR 3-2 hundred 1207.05 km. Average velocity METEOR 3-2 is 26107.87 km/h. Inclination METEOR 3-2 satellite 82.54°.

TLE



Average orbit height METEOR 3-2

Average velocity METEOR 3-2

Average inclination METEOR 3-2

Mean right ascension of the ascending node (RAAN) METEOR 3-2

Mean argument of perigee METEOR 3-2

Mean semi-major axis of the orbit METEOR 3-2

Mean orbital eccentricity METEOR 3-2

Update time: 2026-09-20 19:50:19
Average height of ISS METEOR 3-2 is: 1207.05km
Average velocity METEOR 3-2 is: 26107.87km/h
Average orbit height METEOR 3-2 is: 82.54°
METEOR 3-2 a new group of Starlink satellites has been launched 1988-07-26
METEOR 3-2 is from 13936 days Days in orbit.