Launch Success
Liftoff Time (GMT)
10:49:59
Wednesday September 6, 1989
The Resurs-F1 (17F41) was one of three subseries of the Soviet Resurs-F1 film-return Earth observation satellite family. They were a follow-on to the Fram (Zenit-4MKT) series. The Resurs-F1 satellites were based on the Zenit-4 reconnaisance satellites. They featured a Zenit/Vostok type 2.3 m spherical reentry capsule, which housed the cameras and film, a service module, and an orbital maneuvering module. It was battery powered allowing for 14 days of operations, although up to 10 days on standby could be added. The differences between the 17F40, 17F41, and 17F43 versions are not clear. The Priroda-4 imaging system consisted of a three-channel multispectral system that includes two KFA-1000 cameras and three KATE-200 cameras. The KFA-1000 (SA-20M) cameras with 1000 mm focal length provided stereo images of up to 5 m resolution with a 60 km swath width. It had a capacity of 1800 frames.
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
594th
Mission
31st
Mission of 1989
2313th
Mission
54th
Mission of 1989
74th
Orbital launch attempt