Space · launch vehicle

Zenit-2

OKB-586 RETIRED

At a glance

Launches

Success rate

82.9%

29 ok · 6 failed

Payload to LEO

13,740 kg

Payload to GTO

—

Manufacturer

Yuzhnoye Design Bureau

Status

Retired

First flight

13 Apr 1985

Reusable

Height

57 m

Diameter

3.9 m

Launch mass

459 t

Liftoff thrust

7,300 kN

Stages

Launch cost

—

Booster landings

—

Links

About

Zenit is a family of space launch vehicles designed by the Yuzhnoye Design Bureau in Dnipro, Ukraine, which was then part of the Soviet Union.

Source The Space Devs — Launch Library 2 Last checked 29 Sept 2026