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 first Soyuz-5 / Sunkar suborbital test flight is scheduled for March 3 between 14:00 and 16:00 Moscow Time.
The first suborbital test flight of Soyuz-5 / Sunkar is scheduled for March 3 between 14:00 and 16:00 Moscow Time.
The first Soyuz-5 suborbital test flight is scheduled for March 3 between 14:00 and 16:00 Moscow Time.
The rocket uses new second-stage engines derived from the RD-0124 engine used on Soyuz-2.1b's third stage.
The Soyuz-5 second stage and its mass simulator will reenter and fall into the Pacific Ocean.
The Soyuz 5 stage 2 is initially on a path to 85° inclination before offset thrust steers it to 65° for re-entry.
The Soyuz 5 test mission is a sub-orbital launch.
The Soyuz 5 stage 1 drop zone is about 1,500 km north of Baikonur.
The Soyuz 5 sub-orbital test launch is scheduled for April 2025.
The first Soyuz-5 rocket’s inaugural flight was pushed to April 2 at the earliest.
The Soyuz 5 launch profile appears to include a second-stage de-orbit and re-entry about 115 minutes after lift-off.
A Soyuz-2 launch is planned from the Plesetsk Cosmodrome between April 1 and 15.
The Orel descent module will use solid rocket motors for both vertical and horizontal speed reduction before touchdown, like Soyuz.
The rollout of the first Soyuz-5 rocket to launch pad Site 45 in Baikonur, Kazakhstan was postponed to March 29.
The new Soyuz 5 rocket is scheduled to launch from Baikonur in the next few days.
During the planned Soyuz-2 launch from the Plesetsk Cosmodrome, separating parts of the launch vehicle may fall in the Udorsky Municipal District, the Knyazhpogostsky Municipal District, and the Kortkerossky Municipal District.
The Soyuz launch used a different military-style payload fairing than the Ariane-4-derived 81KS fairing depicted by the satellite developer.
Bureau 1440 separated 16 Rassvet satellites from Soyuz's third stage.
A Bureau 1440 video depicts 16 Rassvet satellites separating from Soyuz's third stage.
The Rassvet satellites were deployed from Soyuz's third stage.