Official name MOLNIYA 1-52
Alternative name Molniya 1-52
Cospar ID 1981-123A
Norad ID 13012
Launch date 1981-12-23
Launch site TTMTR
Launch vehicle Molniya-M (Blok-ML)
Country/Organization USSR
Type application Communication
RCS size LARGE
Decay date ON ORBIT
Period (min) 717.81
Inclination (deg) 61.5
Perigee (km) 1180
Apogee (km) 39176
Eccentricity 0.941520467836257
Mean motion (revs. per day) 2.00610189325866
Semi-Major axis (km) 26556.135
Raan (deg) 182.4129
Arg of perigee (deg) 263.9471
Shape Cyl + 6 Pan
Mass (kg) 1650
Diameter (m) 1.4
Height (m) 4.4
Span (m^2) 8.6
Lifetime 2 years
Contractors NPO Prikladnoi Mekhaniki (NPO PM)
Propulsion KDU-414A (S5.114)
Configuration KAUR-2
Power 6 deployable solar arrays, batteries

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.

The Molniya satellites feature a unique configuration. The pressurized, three-axis stabilized KAUR-2 satellite bus features six non-articulated solar arrays and is operated in a sun-pointed mode. The antennas are mounted on two telescopic arms and are pointable. Each antenna features an optical tracking system which provides information to direct one of the two antennas to the Earth.

The KAUR-2 bus features the KDU-414 propellant system with the S5.31 engine. From 1974 onwards, it was replaced with the KDU-414A with the S5.114 engine in 1974. It is derived from the propulsion system of the Venera 1VA probes.

Molniya-1K for the military telecommunications network Korund carries the Beta communications payload consisting of 5 transponders. It uses wave tubes more reliable than those of Molniya-1's Alfa, which increases the design life of the satellite from one to two years.

Several satellites, beginning with Molniya-1 3, carried an additional earth observation payload called Berkut consisting of two TV cameras, initially black and white, later also colour. This payload was used for meteorology and also for preparation of a early warning system.

Satellite COSPAR Date LS Launch Vehicle Remarks
MOLNIYA 1-26 1973-097A 1973-11-30 PKMTR Molniya-M (Blok-ML)
MOLNIYA 1-30 1975-049A 1975-06-05 PKMTR Molniya-M (Blok-ML) with SRET 2 (MAS 2)
MOLNIYA 1-32 1976-006A 1976-01-22 TTMTR Molniya-M (Blok-ML)
MOLNIYA 1-33 1976-021A 1976-03-11 PKMTR Molniya-M (Blok-ML)
MOLNIYA 1-34 1976-026A 1976-03-19 TTMTR Molniya-M (Blok-ML)
MOLNIYA 1-35 1976-074A 1976-07-23 TTMTR Molniya-M (Blok-ML)
MOLNIYA 1-36 1977-021A 1977-03-24 PKMTR Molniya-M (Blok-ML)
MOLNIYA 1-37 1977-054A 1977-06-24 TTMTR Molniya-M (Blok-ML)
MOLNIYA 1-38 1977-082A 1977-08-30 PKMTR Molniya-M (Blok-ML)
MOLNIYA 1-39 1978-024A 1978-03-02 PKMTR Molniya-M (Blok-ML)
MOLNIYA 1-40 1978-055A 1978-06-02 PKMTR Molniya-M (Blok-ML)
MOLNIYA 1-41 1978-072A 1978-07-14 PKMTR Molniya-M (Blok-ML)
MOLNIYA 1-42 1978-080A 1978-08-22 PKMTR Molniya-M (Blok-ML)
MOLNIYA 1-43 1979-031A 1979-04-12 PKMTR Molniya-M (Blok-ML)
MOLNIYA 1-44 1979-070A 1979-07-31 PKMTR Molniya-M (Blok-ML)
MOLNIYA 1-45 1979-091A 1979-10-20 PKMTR Molniya-M (Blok-ML)
MOLNIYA 1-46 1980-002A 1980-01-11 PKMTR Molniya-M (Blok-ML)
MOLNIYA 1-47 1980-053A 1980-06-21 PKMTR Molniya-M (Blok-ML)
MOLNIYA 1-48 1980-092A 1980-11-16 PKMTR Molniya-M (Blok-ML)
MOLNIYA 1-49 1981-009A 1981-01-30 PKMTR Molniya-M (Blok-ML)
MOLNIYA 1-50 1981-060A 1981-06-24 PKMTR Molniya-M (Blok-ML)
MOLNIYA 1-51 1981-113A 1981-11-17 PKMTR Molniya-M (Blok-ML)
MOLNIYA 1-52 1981-123A 1981-12-23 TTMTR Molniya-M (Blok-ML)
MOLNIYA 1-53 1982-015A 1982-02-26 PKMTR Molniya-M (Blok-ML)
MOLNIYA 1-54 1982-050A 1982-05-28 PKMTR Molniya-M (Blok-ML)
MOLNIYA 1-55 1982-074A 1982-07-21 TTMTR Molniya-M (Blok-ML)
COSMOS 1423 1982-115A 1982-12-08 TTMTR Molniya-M (Blok-ML)
MOLNIYA 1-56 1983-019A 1983-03-16 PKMTR Molniya-M (Blok-ML)
MOLNIYA 1-58 1983-073A 1983-07-19 TTMTR Molniya-M (Blok-ML)
MOLNIYA 1-59 1983-114A 1983-11-23 PKMTR Molniya-M (Blok-ML)
MOLNIYA 1-62 1984-089A 1984-08-24 PKMTR Molniya-M (Blok-ML)