Long March 8A
Profile data last updated: 2026-08-15T20:08:04.839063+00:00 | 7531-09-01
The Long March 8A is an orbital launch vehicle developed by the China Academy of Launch Vehicle Technology based on the Long March 8. It has an increased capability of up to 7 tonnes to a 700 km altitude sun-synchronous orbit. It implements a larger 3.35 meters diameter liquid hydrogen/liquid oxygen 2nd stage, coupled with 2 upgraded version of the YF-75D engines used on the Long March 5 (known as the YF-75H) with increased thrust to 10 tonnes each through measures such as increased turbopump speeds. The Long March 8A can also use a larger 5.2 meters diameter payload fairing.
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 |
|---|---|---|
| Long March 8A | SatNet LEO Group 23 | Aug 04, 2026 08:52 UTC | Success |
| Long March 8A | SpaceSail Polar Group #14 | Jul 05, 2026 13:43 UTC | Success |
| Long March 8A | SatNet LEO Group 20 | Mar 12, 2026 19:48 UTC | Success |
| Long March 8A | SatNet LEO Group 18 | Jan 13, 2026 15:25 UTC | Success |
| Long March 8A | SatNet LEO Group 17 | Dec 25, 2025 23:26 UTC | Success |
| Long March 8A | SatNet LEO Group 14 | Dec 06, 2025 07:53 UTC | Success |
| Long March 8A | SatNet LEO Group 12 | Oct 16, 2025 01:33 UTC | Success |
| Long March 8A | SatNet LEO Group 10 | Aug 25, 2025 19:08 UTC | Success |
| Long March 8A | SatNet LEO Group 06 | Jul 30, 2025 07:49 UTC | Success |
| Long March 8A | SatNet LEO Group 02 (Demo Flight) | Feb 11, 2025 09:30 UTC | Success |