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.
If Baikonur cannot support new Soyuz crew launches for an extended period, Moscow may accelerate work at alternative sites such as Vostochny.
The crew of Soyuz MS-28 includes NASA astronaut Chris Williams and Roscosmos astronauts Sergey Kud-Sverchkov and Sergey Mikayev.
Roscosmos reported damage on several elements of the launch pad used for the Soyuz MS-28 mission after inspections.
The Shenzhou spacecraft is developed from the Russian Soyuz design with significant Chinese modifications.
NASA, Northrop Grumman, and Roscosmos coordinated the move of Cygnus XL to provide clearance for Soyuz MS-28's arrival.
Due to the risk of overheating, the Russian space agency decided to send Soyuz MS-23 to the ISS to bring back the crew from the lightly damaged spacecraft.
The early deployment of Shenzhou-22, originally scheduled for launch in April next year, may be based on the experience of the Russian Soyuz program.
On September 13, Russia launched its Soyuz-2.1b rocket carrying two satellites: a GLONASS satellite and Mozhayets-6.
In December 2022, a micrometeoroid particle impacted the thermal control system radiator of Soyuz MS-22 while aboard the International Space Station (ISS).
The US public catalog of orbital objects listed the upper stage of the Soyuz rocket and the GLONASS payload operating in MEO at 19,100 km above Earth, but did not catalog Mozhayets-6.
The design of the Shenzhou spacecraft is based on that of the Russian Soyuz spacecraft.
Macron called for increasing the frequency of Ariane 6 launches and modernizing the Guiana Space Centre, including renovating the Diamant and Soyuz launch platforms.
The Guiana Space Centre is set to be modernized, including the redevelopment of the Diamant and Soyuz launch pads.
Powers supported six shuttle missions and four Soyuz missions.
Iran's Omid-e-Faza company highlighted the operational achievement of its Kowsar and Hodhod satellites following their launch aboard a Soyuz rocket.
The Soyuz spacecraft will transport humans into orbit until the heat death of the universe.
The Soyuz spacecraft might resume transporting crews to Russia's post-International Space Station.
Soyuz MS-28 has completed testing in an anechoic chamber to test the spacecraft's radio equipment.
After testing, Soyuz MS-28 was placed into the usual workplace for further preparations and tests.
The cash reserve will support the renovation of the old Soyuz launch facility in French Guiana and the inaugural flight of the Maia rocket.