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About this launch
The Molniya were Soviet communication satellites operating from an inclined highly elliptical earth orbit of 500 km × 40000 km with 12 hour period for coverage of high northern latitudes.
More about this launch
Flight profileThe climb, seen from the side · 3D replay on the globe
Launch window and padBaikonur Cosmodrome, Republic of Kazakhstan
- Site
- Baikonur Cosmodrome, Republic of Kazakhstan
Rocket and boosterMolniya-M 2BL
- Vehicle
- Molniya-M 2BL
Molniya-M 2BL: specs, record and next flights → Soviet Union: all its launches →
MissionCommunications · Elliptical
Communications · Elliptical
What it put in orbit6 catalogued objects
| Object | Type | Orbit | Globe |
|---|---|---|---|
| MOLNIYA 1-22 1972-095A | Payload | re-entered 1976-02-11 | |
| SL-6 R/B(1) 1972-095B | Rocket body | re-entered 1973-01-10 | |
| SL-6 PLAT 1972-095C | Debris | re-entered 1973-02-02 | |
| SL-6 DEB 1972-095D | Debris | re-entered 1972-12-12 | |
| SL-6 DEB 1972-095E | Debris | re-entered 1972-12-11 | |
| SL-6 R/B(2) 1972-095F | Rocket body | re-entered 1975-02-25 |
COSPAR ID 1972-095. Orbits from the CelesTrak satellite catalogue (perigee × apogee, inclination).
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