NEXT SPACEFLIGHT

Status

Success

Cosmos 2326

Launch Time
Wed Dec 20, 1995 00:52 UTC

Rocket

Tsyklon-2
VKS RF
Status: Retired
Liftoff Thrust: 2,650 kN
Payload to LEO: 2,850 kg
Payload to GTO: 0 kg
Stages: 2
Strap-ons: 0
Rocket Height: 39.65 m
Fairing Diameter: 3.0 m
Fairing Height: 10.7 m

Mission Details

Cosmos 2326

The US-P and its variant US-PM satellites are a family of Soviet electromagnetic intelligence satellites developed in the 1960s to locate the military ships of enemy fleets by passively listening to the electromagnetic emissions of their electronic equipment. These satellites were used to obtain tactical intelligence and provide target coordinates for air-to-sea and sea-to-ship trans-horizon missiles tasked with sinking the ships. The US-P was designed in the 1960s by OKB-52 and built by KB Arsenal in Leningrad. The first launch took place in 1974 and the system was declared operational in 1978. The data collected by the US-P were complemented by those of the US-A satellites which used an active radar to detect ships in radio silence. From 1993, the US-P was replaced by the US-PM. Russia had only one operational US-PM satellite left in 2014, but it was replaced by the Pion-NKS satellite, launched in 2021.

The US-P satellite is a cylindrical spacecraft with a diameter of 1.3 meters and a mass of 3.3 tons. The body of the satellite is framed by two solar panels one and a half times longer and parallel to it, bringing the total length to 17 meters. The satellite is equipped with an electromagnetic signal detection system. A large X-shaped antenna collects the electromagnetic signals emitted by the enemy fleet. Orbit and orientation corrections are performed with 4 rocket engines of 100 newtons burning a mixture of UDMH and nitrogen peroxide. Ion engines are used for frequent fine adjustments of the orbit. The system was capable of providing data on potential targets with an accuracy of 2 kilometers.

US-P satellites operate in an orbit with an average altitude of 435 km and an inclination of 65°. The average life of a satellite was one and a half years. Given the speed at which ships move, the system had to be able to update the position of targets every two hours so that the coordinates provided to the missile remained usable.

Payloads: 1
Total Mass: 3,300.0 kg
Low Earth Orbit

Location

Site 90/20, Baikonur Cosmodrome, Kazakhstan

Stats

1995

77th orbital launch attempt

Tsyklon-2

100th mission
2nd mission of 1995
96th successful mission
12th consecutive successful mission