Союз
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 |
|---|---|---|
| 2019 | 16 | 0 |
| 2020 | 15 | 0 |
| 2021 | 21 | 0 |
| 2022 | 17 | 0 |
| 2023 | 15 | 0 |
| 2024 | 14 | 0 |
| 2025 | 12 | 0 |
| 2026 | 6 | 8 |
| 2027 | 0 | 8 |
| 2028 | 0 | 8 |
| 2029 | 0 | 8 |
| 2030 | 0 | 8 |
| 2031 | 0 | 8 |
| 2032 | 0 | 8 |
| 2033 | 0 | 8 |
| 2034 | 0 | 8 |
| 2035 | 0 | 8 |
Payload capacity by variant and target orbit when structured capacity rows are available.
| Variant | Orbit | Capacity | Altitude | Inclination | Source |
|---|---|---|---|---|---|
Soyuz-2-1B Союз-2.1б | LEO | 8,320 kg | 200 km | 51.7 deg | RKTs Progress Soyuz-2 page |
Soyuz-2-1B Союз-2.1б | LEO | 8,200 kg | 200 km | 51.8 deg | RKTs Progress Soyuz-2 page |
Latest launched missions using variants in this family.
| Mission | Variant | Launch |
|---|---|---|
| Progress MS-34 Mission | Soyuz-2-1A Союз-2.1а | Apr 25, 2026 |
| Kosmos-2609/2612? | Soyuz-2-1B Союз-2.1б | Apr 16, 2026 |
| Meridian No. 21L? | Soyuz-2-1A Fregat | Apr 3, 2026 |
| Rassvet-3 G1 |
Canonical variants rolled up into this launch vehicle family.
| Variant | Stages | Missions | Status |
|---|---|---|---|
Soyuz-2-1A Союз-2.1а | Not stated | 57 | Active |
Soyuz-2-1A Fregat | Not stated | 23 | Active |
Soyuz-2-1A Volga | Not stated | 1 | Retired |
Soyuz-2-1B Союз-2.1б | Not stated | 24 |
| 2036 | 0 | 8 |
| 2037 | 0 | 8 |
| 2038 | 0 | 8 |
| 2039 | 0 | 8 |
| 2040 | 0 | 8 |
| 2041 | 0 | 8 |
1 launch location represented.
| Year | Location | Launches | Confidence | Basis |
|---|---|---|---|---|
| 2026 | Baikonur Cosmodrome | Site 31/6 | 8 | 30% | Editable low-confidence Soyuz-2/Fregat variant annual throughput default inherited from Soyuz-2 family cadence. |
| 2027 | Baikonur Cosmodrome | Site 31/6 | 8 | 35% | Soyuz-2 active crew/cargo and payload variant; conservative annual rate below historical Soyuz-family ability. |
| 2028 | Baikonur Cosmodrome | Site 31/6 | 8 | 30% | Editable low-confidence Soyuz-2/Fregat variant annual throughput default inherited from Soyuz-2 family cadence. |
| 2029 | Baikonur Cosmodrome | Site 31/6 | 8 | 35% | Soyuz-2 active payload variant; conservative annual rate below historical Soyuz-family ability. |
| 2030 | Baikonur Cosmodrome | Site 31/6 | 8 | 30% | Editable low-confidence Soyuz-2/Fregat variant annual throughput default inherited from Soyuz-2 family cadence. |
| 2031 | Baikonur Cosmodrome | Site 31/6 | 8 | 35% | Soyuz-2 active payload variant; conservative annual rate below historical Soyuz-family ability. |
| 2032 | Baikonur Cosmodrome | Site 31/6 | 8 | 30% | Editable low-confidence Soyuz-2/Fregat variant annual throughput default inherited from Soyuz-2 family cadence. |
| 2033 | Baikonur Cosmodrome | Site 31/6 | 8 | 30% | Editable low-confidence Soyuz-2/Fregat variant annual throughput default inherited from Soyuz-2 family cadence. |
| 2034 | Baikonur Cosmodrome | Site 31/6 | 8 | 30% | Editable low-confidence Soyuz-2/Fregat variant annual throughput default inherited from Soyuz-2 family cadence. |
| 2035 | Baikonur Cosmodrome | Site 31/6 | 8 | 35% | Soyuz-2 active crew/cargo and payload variant; conservative annual rate below historical Soyuz-family ability. |
| 2036 | Baikonur Cosmodrome | Site 31/6 | 8 | 30% | Editable low-confidence Soyuz-2/Fregat variant annual throughput default inherited from Soyuz-2 family cadence. |
| 2037 | Baikonur Cosmodrome | Site 31/6 | 8 | 35% | Soyuz-2 active payload variant; conservative annual rate below historical Soyuz-family ability. |
| 2038 | Baikonur Cosmodrome | Site 31/6 | 8 | 35% | Soyuz-2 active payload variant; conservative annual rate below historical Soyuz-family ability. |
| 2039 | Baikonur Cosmodrome | Site 31/6 | 8 | 30% | Editable low-confidence Soyuz-2/Fregat variant annual throughput default inherited from Soyuz-2 family cadence. |
| 2040 | Baikonur Cosmodrome | Site 31/6 | 8 | 35% | Soyuz-2 active crew/cargo and payload variant; conservative annual rate below historical Soyuz-family ability. |
| 2041 | Baikonur Cosmodrome | Site 31/6 | 8 | 35% | Soyuz-2 active crew/cargo and payload variant; conservative annual rate below historical Soyuz-family ability. Site-year coverage backfill copied nearest prior... |
Editable low-confidence Soyuz-2/Fregat variant annual throughput default inherited from Soyuz-2 family cadence.
Soyuz-2 active crew/cargo and payload variant; conservative annual rate below historical Soyuz-family ability.
Editable low-confidence Soyuz-2/Fregat variant annual throughput default inherited from Soyuz-2 family cadence.
Soyuz-2 active payload variant; conservative annual rate below historical Soyuz-family ability.
Editable low-confidence Soyuz-2/Fregat variant annual throughput default inherited from Soyuz-2 family cadence.
Soyuz-2 active payload variant; conservative annual rate below historical Soyuz-family ability.
Soyuz-2-1A Союз-2.1а | LEO | 7,150 kg | 200 km | 51.7 deg | RKTs Progress Soyuz-2 page |
Soyuz-2-1A Союз-2.1а | LEO | 7,020 kg | 200 km | 51.8 deg | RKTs Progress Soyuz-2 page |
Soyuz-2-1B Fregat | LEO | 6,900 kg | Unknown | Unknown | Manual variant fallback from Soyuz-2-1B family capacity. |
Soyuz-2-1B Союз-2.1б | LEO | 6,900 kg | 200 km | 98.3 deg | RKTs Progress Soyuz-2 page |
Soyuz-2-1B Союз-2.1б | Polar | 6,900 kg | 200 km | 98.3 deg | RKTs Progress Soyuz-2 page |
Soyuz-2-1A Союз-2.1а | Polar | 5,900 kg | 200 km | 98.3 deg | RKTs Progress Soyuz-2 page |
Soyuz-2-1A Fregat | LEO | 5,900 kg | Unknown | Unknown | Manual variant fallback from Soyuz-2-1A family capacity. |
Soyuz-2-1A Союз-2.1а | LEO | 5,900 kg | 200 km | 98.3 deg | RKTs Progress Soyuz-2 page |
Soyuz-2-1B Fregat | SSO | 4,900 kg | 660 km | Unknown | Arianespace Soyuz CSG User's Manual Issue 2.1, May 2018 |
Soyuz-2-1A Fregat | SSO | 4,450 kg | 660 km | Unknown | Arianespace Soyuz CSG User's Manual Issue 2.1, May 2018 |
Soyuz-2-1B Fregat | GTO | 3,250 kg | Unknown | Unknown | Arianespace Soyuz CSG User Manual Issue 2.1 |
Soyuz-2-1B Fregat | TLI | 1,800 kg | Unknown | Unknown | Arianespace Soyuz CSG User Manual; Soyuz/Fregat lunar mission heritage |
Soyuz-2-1B Союз-2.1б | TLI | 1,500 kg | Unknown | Unknown | RKTs Progress Soyuz-2 page |
Soyuz-2-1A Fregat | TLI | 1,500 kg | Unknown | Unknown | Arianespace Soyuz CSG User Manual; Soyuz/Fregat high-energy mission heritage |
Soyuz-2-1B Союз-2.1б |
| Mar 23, 2026 |
| Progress MS-33 Mission | Soyuz-2-1A Союз-2.1а | Mar 22, 2026 |
| Kosmos-2600-2608? | Soyuz-2-1B Fregat | Feb 5, 2026 |
| Aist-2T No. 1/2 | Soyuz-2-1B Fregat | Dec 28, 2025 |
| Obzor-R No. 1 Mission | Soyuz-2-1A Союз-2.1а | Dec 25, 2025 |
Upcoming mission rows with announced launch timing.
| Mission | Variant | Announced |
|---|---|---|
No forecasted missionsNo upcoming announced mission rows are linked to this vehicle family. | ||
| Active |
Soyuz-2-1B Fregat | Not stated | 59 | Active |
Soyuz-FG | Not stated | 60 | Retired |
Soyuz-FG Fregat | Not stated | 10 | Retired |
Soyuz-ST-A Fregat | Not stated | 9 | Retired |
Soyuz-ST-B Fregat | Not stated | 18 | Retired |
Soyuz-U | Not stated | 633 | Retired |
Soyuz-U2 | Not stated | 72 | Retired |
Soyuz-U-PVB | Not stated | 144 | Retired |
Soyuz-U-PVB Fregat | Not stated | 4 | Retired |
Soyuz-U-PVB Ikar | Not stated | 6 | Retired |
Editable low-confidence Soyuz-2/Fregat variant annual throughput default inherited from Soyuz-2 family cadence.
Editable low-confidence Soyuz-2/Fregat variant annual throughput default inherited from Soyuz-2 family cadence.
Editable low-confidence Soyuz-2/Fregat variant annual throughput default inherited from Soyuz-2 family cadence.
Soyuz-2 active crew/cargo and payload variant; conservative annual rate below historical Soyuz-family ability.
Editable low-confidence Soyuz-2/Fregat variant annual throughput default inherited from Soyuz-2 family cadence.
Soyuz-2 active payload variant; conservative annual rate below historical Soyuz-family ability.
The retirement of the Ariane 5, the loss of access to the Soyuz rocket after Russia’s invasion of Ukraine, and delays in the introduction of the Ariane 6 left Europe without its own means of launching Galileo satellites.
Twenty-eight Galileo satellites had launched to date prior to the Galileo L12 mission, all of them on Russian-built Soyuz rockets or Europe’s Ariane 5.
Soyuz MS-24 will perform a parachute-assisted landing on the steppe of Kazakhstan on 2024-04-06.
The hatches between the International Space Station and Soyuz MS-25 are scheduled to open at about 1:40 p.m. on 2024-03-25.
Soyuz MS-25 will dock to the International Space Station’s Prichal module at about 11:09 a.m. on Monday, 2024-03-25.
NASA astronaut Loral O’Hara launched to the station in Soyuz MS-24 in September with Russian cosmonauts Oleg Kononenko and Nikolai Chub.
Roscosmos cosmonauts Oleg Kononenko and Nikolai Chub, who launched on Soyuz MS-24, will remain on the International Space Station for an additional six months.
Roscosmos prepares to launch the meteorological satellite Meteor-M 2-4 on a Soyuz 2.1b rocket.
Accusations of racism arose following Jeanette Epps' reassignment from the 2018 Soyuz mission, although she stated she had no issues working with Russians.
Jeanette Epps was originally selected for a Soyuz mission to the ISS in 2018 but was reassigned just months before launch.
Dr. Soichi Noguchi flew as the first Japanese 'left-seater' on the Soyuz spacecraft in 2009.
The international Soyuz crew launched on Soyuz MS-22 in September 2022 with Frank Rubio, Sergey Prokopyev, and Dmitri Petelin.
The Soyuz crew spent 371 days aboard the International Space Station.
The Soyuz crew served on Expeditions 68 and 69 aboard the International Space Station.
The Soyuz-2.1a rocket used for Progress MS-25 is decorated with depictions commemorating the 35th anniversary of the Buran reusable space shuttle flight.
The Progress MS-25 resupply ship launched on a Soyuz-2.1a carrier rocket from the Baikonur Cosmodrome in Kazakhstan on 2023-12-01.
The entire Soyuz rocket collapsed and exploded back onto the launch pad just after the crew's escape.
The Soyuz descent module landed approximately 3.7 kilometers from the launch pad.
Discussions to use a non-European rocket such as Falcon 9 for Galileo launches occurred because of delays in Ariane 6, the retirement of Ariane 5, and the withdrawal of Soyuz following Russia’s invasion of Ukraine.
Soyuz-T-10 was the second use of a launch abort system, following the first use nearly a decade earlier during the Soyuz 7K-T No.39 mission.