Soyuz
In-activeMinistry of Defence of the Russian Federation (MOD_RUS)
March 29, 2018
Description
Specifications
-
Stages
2 -
Length
44.0 m -
Diameter
3.0 m -
Fairing Diameter
― -
Launch Mass
158.0 T -
Thrust
―
Family
-
Name
Soyuz -
Family
― -
Variant
2.1v -
Alias
― -
Full Name
Soyuz 2.1v
Payload Capacity
-
Launch Cost
― -
Low Earth Orbit
2850.0 kg -
Geostationary Transfer
Orbit
― -
Direct Geostationary
― -
Sun-Synchronous Capacity
―
Ministry of Defence of the Russian Federation
Government
Minister: Gen. Sergey Shoygu
MOD_RUS 1717The Ministry of Defence of the Russian Federation is the governing body of the Russian Armed Forces.
Soyuz 2.1v | Kosmos 2575
Ministry of Defence of the Russian Federation | RussiaPlesetsk Cosmodrome, Russian Federation
Feb. 9, 2024, 7:03 a.m.
Soyuz 2.1v | Kosmos 2574
Ministry of Defence of the Russian Federation | RussiaPlesetsk Cosmodrome, Russian Federation
Dec. 27, 2023, 7:03 a.m.
Soyuz 2.1v | Razbeg 1 (Kosmos 2551)
Ministry of Defence of the Russian Federation | RussiaPlesetsk Cosmodrome, Russian Federation
Sept. 9, 2021, 7:59 p.m.
Status: Launch Successful
Mission:
The Russian Razbeg 1 is small military satellite optical reconnaissance satellite. It was built by NPP VNIIEM. It is likely the same satellite identified in earlier reports as Zvesda. The 250 kg satellite was reportedly inspired by the US American commercial Earth imaging satellites of the SkySat 1 series. It features a camera built by the Belarusian company OAO Peleng with a maximum ground resolution of 0.9 meters in panchromatic mode.
Sun-Synchronous OrbitSoyuz 2.1v | VNIIEM EMKA (Kosmos 2525)
Ministry of Defence of the Russian Federation | RussiaPlesetsk Cosmodrome, Russian Federation
March 29, 2018, 5:38 p.m.
Status: Launch Successful
Mission:
The payload for the Soyuz-2-1v launch is a small reconnaissance satellite developed by VNIIEM and known by the acronym EMKA ("Experimental Small Space Apparatus"). Launch was originally scheduled for October and then slipped to November, December and eventually January due to technical problems with the payload.
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