Soyuz STA Fregat
Profile data last updated: 2026-08-15T20:08:04.839063+00:00 | 7531-09-01
The 2.1a version includes conversion from analog to digital flight control system and uprated engines on the booster and the first stage with improved injection systems. The new digital flight control and telemetry systems allow the rocket to launch from a fixed rather than angled launch platform and adjust its heading in flight. A digital control system also enables the launch of larger commercial satellites with wider and longer payload fairings such as the ST-type fairing. These fairings introduce too much aerodynamic instability for the old analog system to handle. This stage continues to use the RD-0110 engine. The 2.1a/ST version is sometimes called Soyuz ST-A.
Specifications
Payload Capacity
Lifetime Launch Record
As reported by Launch Library 2 across this rocket's entire history, not just the launches tracked on this site.
Launches Tracked on This Site
| Mission | Date | Status |
|---|---|---|
| Soyuz STA/Fregat | CSO-2 | Dec 29, 2020 16:42 UTC | Success |
| Soyuz STA/Fregat | Falcon Eye 2 | Dec 02, 2020 01:33 UTC | Success |
| Soyuz STA/Fregat | CSO-1 | Dec 19, 2018 16:37 UTC | Success |
| Soyuz STA/Fregat | SES-15 | May 18, 2017 11:54 UTC | Success |
| Soyuz STA/Fregat | Sentinel-1B | Apr 25, 2016 21:02 UTC | Success |
| Soyuz STA/Fregat | Sentinel-1A | Apr 03, 2014 21:02 UTC | Success |
| Soyuz STA/Fregat | Pléiades-HR 1B | Dec 02, 2012 02:02 UTC | Success |
| Soyuz STA/Fregat | Pléiades-HR 1A, FASat-Charlie (SSOT), 4 x ELISA | Dec 17, 2011 02:03 UTC | Success |