MOLNIYA 1-80
Satellite information MOLNIYA 1-80 - Molniya-1
| Spacetrack Directory Name | MOLNIYA 1-80 |
| Alternative name | Molniya-1 |
| Group | MOLNIYA |
| Follow MOLNIYA 1-80 | MOLNIYA 1-80 Tracker |
| Group follow MOLNIYA | Tracker MOLNIYA |
| Pass predictions MOLNIYA 1-80 | Pass predictions MOLNIYA 1-80 |
| Orbit launches |
1991-02-15 (35 years ago)
|
| Days in orbit | 13001 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | PLMSC (Plesetsk Missile and Space Complex, Russia) |
| Type | Satellite |
| Categories | |
| Perigee | 1789 km |
| Apogee | 37765 km |
| Orbit slope (inclination) | 64.89° |
| Laps per day | 2 |
| Height MOLNIYA 1-80 | 25032.34 km |
Additional information MOLNIYA 1-80
The MOLNIYA 1-80 satellite, also known as Molniya-1, was launched on February 15, 1991, from the Plesetsk Cosmodrome LC43/3 launch pad using a Molniya 8K78M launch vehicle. It belongs to the Molniya-1T series and has a configuration known as KAUR-2. With dimensions of 4.4 meters in length and 1.4 meters in diameter, it also features an 8.6-meter span due to its solar arrays. The satellite had a dry mass of 1620 kilograms and a launch mass of 1670 kilograms. Its purpose was for communication, and it was equipped with six deployable solar arrays and batteries for power. The spacecrafts shape is cylindrical with six panels, and it has an RCS value of 10. MOLNIYA 1-80 was manufactured by NPOPM (NPO Mashinostroyeniya) and operated for a lifetime of approximately three years. Its motor type is the KDU-414A (S5.114). The satellites payload is identified as Molniya-1T No. 89L, and it was owned by UNKSR.
satellite MOLNIYA 1-80 Date of exalting 15.02.1991y. Average height of ISS MOLNIYA 1-80 hundred 25032.34 km. Average velocity MOLNIYA 1-80 is 12516.89 km/h. Inclination MOLNIYA 1-80 satellite 64.89°.TLE
Average velocity MOLNIYA 1-80
Average inclination MOLNIYA 1-80
Mean right ascension of the ascending node (RAAN) MOLNIYA 1-80
Mean argument of perigee MOLNIYA 1-80
Mean semi-major axis of the orbit MOLNIYA 1-80
Mean orbital eccentricity MOLNIYA 1-80
ISS
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