Launch Success
Liftoff Time (GMT)
07:45:00
Friday August 17, 1979
Zenit was a series of military photoreconnaissance satellites launched by the Soviet Union between 1961 and 1994. The basic design of the Zenit satellites was similar to the Vostok crewed spacecraft, sharing the return and service modules. It consisted of a spherical re-entry capsule 2.3 metres in diameter with a mass of around 2,400 kilograms. This capsule contained the camera system, its film, recovery beacons, parachutes and a destruct charge. In orbit, this was attached to a service module that contained batteries, electronic equipment, an orientation system and a liquid fuelled rocket engine that would slow the Zenit for re-entry, before the service module detached. The total length in orbit was around 5 metres. Unlike the American Corona spacecraft, the return capsule carried both the film and the cameras and kept them in a temperature controlled pressurised environment. This simplified the design and engineering of the camera system but added considerably to the mass of the satellite. An advantage was that cameras could be reused. Most Zenits flew in a slightly elliptical orbit with a perigee of around 200 kilometres (120 miles) and an apogee between 250 and 350 kilometres (160 and 220 miles); the missions usually lasted between 8 and 15 days.
Low Earth Orbit
1 Payload
6,300 kilograms
Manufacturer
RKK EnergiyaPrice
$20.00 million
Rocket
Height: 51.32m
Payload to Orbit
LEO: 6,860 kg
GTO: 0 kg
Liftoff Thrust
4,456 Kilonewtons
Fairing
Diameter: 3m
Height: 15.59m
Stages
3
Strap-ons
4
165th
Mission
34th
Mission of 1979
1345th
Mission
63rd
Mission of 1979
78th
Orbital launch attempt