MOLNIYA 1-86
Satellite information MOLNIYA 1-86 - Molniya-1
| Spacetrack Directory Name | MOLNIYA 1-86 |
| Alternative name | Molniya-1 |
| Group | MOLNIYA |
| Follow MOLNIYA 1-86 | MOLNIYA 1-86 Tracker |
| Group follow MOLNIYA | Tracker MOLNIYA |
| Pass predictions MOLNIYA 1-86 | Pass predictions MOLNIYA 1-86 |
| Orbit launches |
1993-05-26 (33 years ago)
|
| Days in orbit | 12169 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | PLMSC (Plesetsk Missile and Space Complex, Russia) |
| Type | Satellite |
| Categories | |
| Perigee | 498 km |
| Apogee | 13452 km |
| Orbit slope (inclination) | 62.93° |
| Laps per day | 6 |
| Height MOLNIYA 1-86 | 8557.41 km |
Additional information MOLNIYA 1-86
MOLNIYA 1-86, also known as Molniya-1, is a communication satellite launched by VKS on May 26, 1993, from the PLMSC launch site using a Molniya 8K78M launch vehicle at LC43/4. The spacecraft has dimensions of 4.4 meters in length and 1.4 meters in diameter, with a span of 8.6 meters and a dry mass of 1,620 kilograms. It is configured as KAUR-2 and operates on a Molniya-1T bus manufactured by NPOPM. The satellites power system consists of six deployable solar arrays and batteries, while its propulsion is provided by the KDU-414A (S5.114) motor. MOLNIYA 1-86 has an expected lifetime of three years and was launched with a mass of 1,670 kilograms. Its shape includes a cylindrical body plus six panels.
satellite MOLNIYA 1-86 Date of exalting 26.05.1993y. Average height of ISS MOLNIYA 1-86 hundred 8557.41 km. Average velocity MOLNIYA 1-86 is 18438.57 km/h. Inclination MOLNIYA 1-86 satellite 62.93°.TLE
Average velocity MOLNIYA 1-86
Average inclination MOLNIYA 1-86
Mean right ascension of the ascending node (RAAN) MOLNIYA 1-86
Mean argument of perigee MOLNIYA 1-86
Mean semi-major axis of the orbit MOLNIYA 1-86
Mean orbital eccentricity MOLNIYA 1-86
ISS
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