Family-level launch record combining canonical variants, historical missions, public cadence forecasts, and available payload performance specs.
Historical missions are grouped by actual launch year. Forecast cadence uses family-level launch-rate rows.
| Year | Historical missions | Forecast launches |
|---|---|---|
| 2008 | 6 | 0 |
| 2009 | 4 | 0 |
| 2011 | 5 | 0 |
| 2012 | 3 | 0 |
| 2013 | 2 | 0 |
| 2014 | 1 | 0 |
| 2015 | 1 | 0 |
| 2017 | 1 | 0 |
Payload capacity by variant and target orbit when structured capacity rows are available.
| Variant | Orbit | Capacity | Altitude | Inclination | Source |
|---|---|---|---|---|---|
No performance specsNo structured payload capacity rows are linked to this vehicle family. | |||||
Latest launched missions using variants in this family.
| Mission | Variant | Launch |
|---|---|---|
| Angosat | Zenit-3SLBF | Dec 26, 2017 |
| Elektro-L No. 2 Mission | Zenit-3SLBF | Dec 11, 2015 |
| Eutelsat 3B | Zenit-3SL | May 26, 2014 |
| Amos 4 Mission |
Canonical variants rolled up into this launch vehicle family.
| Variant | Stages | Missions | Status |
|---|---|---|---|
Zenit-2 | Not stated | 34 | Retired |
Zenit-2 11K77.05 | Not stated | 1 | Retired |
Zenit-2M | Not stated | 1 | Retired |
Zenit-2SB | Not stated | 1 | Retired |
Zenit-3SLB |
| Aug 31, 2013 |
| Launch 2013-F01 | Zenit-3SL | Feb 1, 2013 |
| SL50 Eutelsat 70B | Zenit-3SL | Dec 3, 2012 |
| SL49 Intelsat IS-21 | Zenit-3SL | Aug 19, 2012 |
| SL45 Intelsat IS-19 | Zenit-3SL | Jun 1, 2012 |
Upcoming mission rows with announced launch timing.
| Mission | Variant | Announced |
|---|---|---|
No forecasted missionsNo upcoming announced mission rows are linked to this vehicle family. | ||
Zenit-3SL | Not stated | 36 | Retired |
Zenit-3SLB | Not stated | 6 | Retired |
Zenit-3SLBF | Not stated | 4 | Retired |
Kazakhstan transported a training version of the Zenit rocket to Site 1 (Gagarin's Start).
The Baiterek project aims to modernize the Zenit-M launch pad at Baikonur and build advanced, sustainable facilities for medium-class spacecraft.
Russia intends Soyuz 5 to replace the Ukrainian-built Zenit family of medium-class launch vehicles.
The revised Science Power Platform design was planned to fly on Zenit launch vehicles with Progress-derived tugs.
Zenit-3F is designed to deliver about 13 to 14 tonnes to low Earth orbit.
Zenit-3F is developed by Yuzhmash.
Soyuz-5 uses Zenit's existing infrastructure.
Soyuz-5 and Zenit share the same launch pad.
Soyuz-5 and Zenit have the same first-stage engine skirt.
Zenit-3F uses an RD-171M first-stage engine burning kerosene and liquid oxygen.
Zenit-3F had a first flight in 1985.
Soyuz-5 uses the same engine as Zenit.
The first-stage engine skirt of Soyuz-5 was copied from Zenit to allow Soyuz-5 to use existing infrastructure.
A rocket with a tapered aft section is being positioned to fit Baikonur Cosmodrome’s Site 45/1 Zenit pad.
The rocket has a larger diameter than Zenit.
Baikonur Cosmodrome’s Site 45/1 is an existing Zenit launch pad.
The Not-Zenit rocket has not yet rolled out to Launch Pad Site 45/1, the former Zenit pad at Baikonur.
Baikonur Site 45 includes a Manned Spacecraft Servicing Unit built to service the Zarya-Zenit stack.
The Zarya spacecraft was designed to use the Zenit launch vehicle.
The Zenit launch vehicle would deliver Zarya to a 190-kilometer reference orbit at an inclination of 51.6 degrees in the 15-tonne configuration.