长征八号
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 |
|---|---|---|
| 2020 | 1 | 0 |
| 2022 | 1 | 0 |
| 2024 | 1 | 0 |
| 2025 | 7 | 0 |
| 2026 | 6 | 8 |
| 2027 | 0 | 12 |
| 2028 | 0 | 16 |
| 2029 | 0 | 20 |
| 2030 | 0 | 24 |
| 2031 | 0 | 24 |
| 2032 | 0 | 24 |
| 2033 | 0 | 24 |
| 2034 | 0 | 24 |
| 2035 | 0 | 24 |
| 2036 | 0 | 24 |
| 2037 | 0 | 24 |
| 2038 | 0 | 24 |
Payload capacity by variant and target orbit when structured capacity rows are available.
| Variant | Orbit | Capacity | Altitude | Inclination | Source |
|---|---|---|---|---|---|
Long March 8A | LEO | 9,800 kg | Unknown | Unknown | Space Launch Now Long March 8A vehicle page |
Long March 8 | LEO | 7,600 kg | Unknown | Unknown | Ed Kyle Space Launch Report CZ-5/6/7/8 summary |
Latest launched missions using variants in this family.
| Mission | Variant | Launch |
|---|---|---|
| Qianfan Xingzuo 15 | Long March 8A | Jul 5, 2026 |
| Qianfan Xingzuo 12 | Long March 8 | Jun 5, 2026 |
| Qianfan Xingzuo 09 | Long March 8 | May 17, 2026 |
| Qianfan Xingzuo 07 |
Canonical variants rolled up into this launch vehicle family.
| Variant | Stages | Missions | Status |
|---|---|---|---|
Long March 8 | Not stated | 6 | Active |
Long March 8 0 | Not stated | 1 | Active |
Long March 8A | Not stated | 9 | Active |
| 2039 | 0 | 24 |
| 2040 | 0 | 24 |
| 2041 | 0 | 24 |
1 launch location represented.
| Year | Location | Launches | Confidence | Basis |
|---|---|---|---|---|
| 2026 | Wenchang Space Launch Site | 8 | 22% | China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume con... |
| 2027 | Wenchang Space Launch Site | 12 | 22% | China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume con... |
| 2028 | Wenchang Space Launch Site | 16 | 22% | China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume con... |
| 2029 | Wenchang Space Launch Site | 20 | 22% | China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume con... |
| 2030 | Wenchang Space Launch Site | 24 | 22% | China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume con... |
| 2031 | Wenchang Space Launch Site | 24 | 22% | China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume con... |
| 2032 | Wenchang Space Launch Site | 24 | 22% | China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume con... |
| 2033 | Wenchang Space Launch Site | 24 | 22% | China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume con... |
| 2034 | Wenchang Space Launch Site | 24 | 22% | China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume con... |
| 2035 | Wenchang Space Launch Site | 24 | 22% | China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume con... |
| 2036 | Wenchang Space Launch Site | 24 | 22% | China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume con... |
| 2037 | Wenchang Space Launch Site | 24 | 22% | China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume con... |
| 2038 | Wenchang Space Launch Site | 24 | 22% | China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume con... |
| 2039 | Wenchang Space Launch Site | 24 | 22% | China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume con... |
| 2040 | Wenchang Space Launch Site | 24 | 22% | China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume con... |
| 2041 | Wenchang Space Launch Site | 24 | 22% | China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume con... |
China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume constellation deploymen...
China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume constellation deploymen...
China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume constellation deploymen...
China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume constellation deploymen...
China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume constellation deploymen...
Long March 8 0 | LEO | 7,600 kg | Unknown | Unknown | Ed Kyle Space Launch Report CZ-5/6/7/8 summary copied from sibling Chang Zheng 8 row |
Long March 8A | SSO | 7,000 kg | 700 km | Unknown | CASC Long March 8A rollout report |
Long March 8 | SSO | 4,500 kg | 700 km | Unknown | CNSA Long March 8 page |
Long March 8 0 | SSO | 4,500 kg | 700 km | Unknown | CNSA Long March 8 page copied from sibling Chang Zheng 8 row |
Long March 8A | GTO | 3,500 kg | Unknown | Unknown | Space Launch Now Long March 8A vehicle page |
Long March 8 0 | GTO | 2,500 kg | Unknown | Unknown | Ed Kyle Space Launch Report CZ-5/6/7/8 summary copied from sibling Chang Zheng 8 row |
Long March 8 | GTO | 2,500 kg | Unknown | Unknown | Ed Kyle Space Launch Report CZ-5/6/7/8 summary |
Long March 8 |
| Apr 7, 2026 |
| WHDW 20 | Long March 8A | Mar 12, 2026 |
| WHDW 18 | Long March 8A | Jan 13, 2026 |
| WHDW 17 | Long March 8A | Dec 25, 2025 |
| WHDW 14 | Long March 8A | Dec 6, 2025 |
Upcoming mission rows with announced launch timing.
| Mission | Variant | Announced |
|---|---|---|
No forecasted missionsNo upcoming announced mission rows are linked to this vehicle family. | ||
China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume constellation deploymen...
China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume constellation deploymen...
China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume constellation deploymen...
China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume constellation deploymen...
China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume constellation deploymen...
China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume constellation deploymen...
China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume constellation deploymen...
The Long March 8A was carrying the eighteenth group of GuoWang satellites, deploying nine from its second stage.
The idea of using a barge for landing Long March 8 rockets was scrapped in favor of starting with the Long March 10 series.
The Long March 8A can carry 3,500 kilograms to geostationary transfer orbit.
The core of the Long March 8A is 50.5 meters tall and weighs 371,000 kilograms when fully fueled.
The Long March 8A is projected to conduct a higher density of missions in 2026, with a potential of up to fifteen more flights this year.
The Long March 8A lifted off at 23:25 pm China Standard Time on January 13th from Commercial Launch Pad 1 at the Wenchang Commercial Space Launch Site.
The Long March 8A mission took place eighteen days after the previous launch, facilitated by optimized launch preparations.
The Long March 8A's first stage is powered by two YF-100 engines, producing a total thrust of 490 tons at liftoff.
The Long March 8 series was CASC/CALT's first point of entry for reusing orbital rockets.
The Long March 8A has a payload capacity of 9,800 kilograms to low Earth orbit.
Long March 8A launched SatNet LEO Group 18 at 15:25 UTC on January 13, 2026 from Hainan, China.
The second stage of the Long March 8A is equipped with two YF-75DA engines that produce 20 tons of thrust.
The Long March 8A is launched from the Wenchang Space Launch Site and the Wenchang Commercial Space Launch Site in Hainan province.
The January 13th launch was the 7th launch of the Long March 8A vehicle and the 625th launch in the Long March series.
The Long March 8A utilizes a two-and-a-half-stage design and is fueled by rocket-grade kerosene and liquid oxygen in the first stage, along with liquid hydrogen and liquid oxygen in the second stage.
The Long March 8A can carry 7,000 kilograms to a 700-kilometer sun-synchronous orbit and 6,800 kilograms to a 900-kilometer sun-synchronous orbit.
Long March 8A Y6 launched SatNet LEO Group 17 at 23:26 UTC on December 25, 2025 from Hainan commercial launch pad #1.
The Long March 8A was on the launch pad for five days prior to the mission, compared to ten days previously for testing and preparations.
The Long March 8A was launched from Wenchang on Christmas Day.
Flight data for the Long March 10 series launch vehicles' engines has been gathered using the YF-100K on the Long March 12 and the YF-75DA on the Long March 8A.