Long March 8A
Long March familyChina Aerospace Science and Technology CorporationActive
Long March 8A | SatNet LEO Group TBD?
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
- Thrust
- 4,800 kN
- Height
- 50.5 m
- Diameter
- 3.35 m
- Launch mass
- 371 t
- Stages
- 2
- LEO capacity
- 9,800 kg
- GTO capacity
- 3,500 kg
- SSO capacity
- 7,000 kg
Specifications from Launch Library. Figures the operator has not published are omitted.
Flight record
First flight February 11, 2025 · 09:30 UTC · latest October 25, 2026 · 02:03 UTC
Counted from padside's own launch record, the same basis as the stats page.
Flights per year
- Successful
- Failed
Show the numbers for Long March 8A flights per year
| Year | Successful | Failed | Total |
|---|---|---|---|
| 2025 | 6 | 0 | 6 |
| 2026 | 6 | 0 | 6 |
Flights
5 of 12- Long March 8A | SatNet LEO Group 28SuccessOct 25 · 02:03 UTC
- Long March 8A | SatNet LEO Group 26SuccessSep 23 · 13:32 UTC
- Long March 8A | SatNet LEO Group 23SuccessAug 04 · 08:52 UTC
- Long March 8A | SpaceSail Polar Group #14SuccessJul 05 · 13:43 UTC
- Long March 8A | SatNet LEO Group 20SuccessMar 12 · 19:48 UTC