Molniya-1 3

Success Soviet Union, Molniya 8K78

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

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Rocket and boosterMolniya 8K78
MissionCommunications · Elliptical

Communications · Elliptical

What it put in orbit6 catalogued objects
ObjectTypeOrbitGlobe
MOLNIYA 1-3 1966-035A Payload re-entered 1973-06-11
SL-6 PLAT 1966-035B Debris re-entered 1966-05-09
SL-6 R/B(1) 1966-035C Rocket body re-entered 1966-05-08
SL-6 DEB 1966-035D Debris re-entered 1966-04-29
SL-6 DEB 1966-035E Debris re-entered 1966-04-29
SL-6 R/B(2) 1966-035F Rocket body re-entered 1973-06-18

COSPAR ID 1966-035. Orbits from the CelesTrak satellite catalogue (perigee × apogee, inclination).

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