Official name COSMOS 1426
Alternative name Cosmos-1426
Cospar ID 1982-120A
Norad ID 13745
Launch date 1982-12-28
Launch site TTMTR
Launch vehicle Soyuz-U
Country/Organization USSR
Type application Reconnaissance, photo (data transmitting)
Operator GRU
RCS size LARGE
Decay date 1983-03-05
Shape Sphere + Cyl
Mass (kg) 6640.24
Diameter (m) 2.7
Height (m) 6.99
Span (m^2) 8.5
Contractors TsSKB
Configuration Yantar Bus
Power 2 deployable solar arrays, batteries

The Terilen or Yantar-4KS1 satellites were the first series of soviet elctro-optical reconnaissance satellites. They transmitted the data via Potok (Geizer) relay satellites.

The Yantar-2K (Feniks) was not capable of providing strategic warning of attack and fast reaction due to the need to return the film. Therefore additional variants were developed, one of them the detailed electro-optical and operational reconnaissance satellite Yantar-4KS. The spacecraft was designed to relay visual and infrared band images via a digital data link to the planned Potok-Luch GKRSS relay satellite system.

There were two phases to the project plan. The first phase spacecraft, the Yantar-4KS1 (Terilen), would be launched by the Soyuz-U launch vehicle, begin flight trials of system components in 1979, with the system to be accepted into the military by 1981. Phase 2 would be the more capable Yantar-4KS2, launched by the more powerful Zenit-2 launch vehicle, with flight trials to begin in 1983.

Soviet digital electronics technology hampered a fast development. The structure and wire harnesses for the first spacecraft were completed in 1978, but delays in the electronics meant that the first flight could not begin until the end of 1982. But the very first trials flight, in conjunction with the first Potok communications relay satellite, proved the worth of the system, with immediate operational use of the imagery. Yantar-4KS1 was accepted into military service in 1985.

On 1 June 1983 the Yantar-4KS2 was cancelled and it was decided to modernise the Yantar-4KS1 instead forming the Yantar-4KS1M (Neman).

Typical orbital profile of the satellites was: inclination 64.9 degrees with an altitude of 230-280 km or 180-270 km.

Satellite COSPAR Date LS Launch Vehicle Remarks
COSMOS 1426 1982-120A 1982-12-28 TTMTR Soyuz-U
COSMOS 1552 1984-045A 1984-05-14 TTMTR Soyuz-U
COSMOS 1643 1985-026A 1985-03-25 TTMTR Soyuz-U
COSMOS 1731 1986-013A 1986-02-07 TTMTR Soyuz-U
COSMOS 1770 1986-060A 1986-08-06 TTMTR Soyuz-U
COSMOS 1810 1986-102A 1986-12-26 TTMTR Soyuz-U
COSMOS 1836 1987-033A 1987-04-16 TTMTR Soyuz-U
COSMOS 1881 1987-076A 1987-09-11 TTMTR Soyuz-U
COSMOS 1936 1988-027A 1988-03-30 TTMTR Soyuz-U
COSMOS 2007 1989-024A 1989-03-23 TTMTR Soyuz-U
COSMOS 2049 1989-088A 1989-11-17 TTMTR Soyuz-U
COSMOS 2072 1990-033A 1990-04-13 TTMTR Soyuz-U
COSMOS 2113 1990-113A 1990-12-21 TTMTR Soyuz-U