MOLNIYA 1-53
Satellite information MOLNIYA 1-53 - Molniya-1
| Spacetrack Directory Name | MOLNIYA 1-53 |
| Alternative name | Molniya-1 |
| Group | MOLNIYA |
| Follow MOLNIYA 1-53 | MOLNIYA 1-53 Tracker |
| Group follow MOLNIYA | Tracker MOLNIYA |
| Pass predictions MOLNIYA 1-53 | Pass predictions MOLNIYA 1-53 |
| Orbit launches |
1982-02-26 (44 years ago)
|
| Days in orbit | 16282 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | PLMSC (Plesetsk Missile and Space Complex, Russia) |
| Type | Satellite |
| Categories | |
| Perigee | 582 km |
| Apogee | 39725 km |
| Orbit slope (inclination) | 63.93° |
| Laps per day | 2 |
| Height MOLNIYA 1-53 | 26894.44 km |
Additional information MOLNIYA 1-53
MOLNIYA 1-53, also known as Molniya-1, is a communication satellite launched on February 26, 1982, from the Plesetsk Cosmodrome using a Molniya 8K78M launch vehicle from Launch Pad LC41/1. The satellite was manufactured by NPOPM and operated for approximately two years under the ownership of GUKOS. It has dimensions of 4.4 meters in length, 1.4 meters in diameter, and an 8.6-meter span. The spacecraft had a launch mass of 1650 kg and a dry mass of 1620 kg. MOLNIYA 1-53 was powered by six deployable solar arrays and batteries, and its shape is described as cylindrical with six panels. It used the KDU-414A (S5.114) motor for propulsion. The satellites primary purpose was communication in orbit.
satellite MOLNIYA 1-53 Date of exalting 26.02.1982y. Average height of ISS MOLNIYA 1-53 hundred 26894.44 km. Average velocity MOLNIYA 1-53 is 11971.64 km/h. Inclination MOLNIYA 1-53 satellite 63.87°.TLE
Average velocity MOLNIYA 1-53
Average inclination MOLNIYA 1-53
Mean right ascension of the ascending node (RAAN) MOLNIYA 1-53
Mean argument of perigee MOLNIYA 1-53
Mean semi-major axis of the orbit MOLNIYA 1-53
Mean orbital eccentricity MOLNIYA 1-53
ISS
Buy us a coffee!
