长征六号
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 |
|---|---|---|
| 2019 | 1 | 0 |
| 2020 | 1 | 0 |
| 2021 | 4 | 0 |
| 2022 | 4 | 0 |
| 2023 | 3 | 0 |
| 2024 | 8 | 0 |
| 2025 | 11 | 0 |
| 2026 | 7 | 10 |
| 2027 | 0 | 12 |
| 2028 | 0 | 14 |
| 2029 | 0 | 16 |
| 2030 | 0 | 16 |
| 2031 | 0 | 16 |
| 2032 | 0 | 16 |
| 2033 | 0 | 16 |
| 2034 | 0 | 16 |
| 2035 | 0 | 16 |
Payload capacity by variant and target orbit when structured capacity rows are available.
| Variant | Orbit | Capacity | Altitude | Inclination | Source |
|---|---|---|---|---|---|
Long March 6A | LEO | 8,000 kg | Unknown | Unknown | Long March 6A public performance profile |
Long March 6A | SSO | 6,500 kg | 500 km | Unknown | Long March 6A public performance profile |
Latest launched missions using variants in this family.
| Mission | Variant | Launch |
|---|---|---|
| Qianfan Xingzuo 13 | Long March 6A | Jul 4, 2026 |
| Qianfan Xingzuo 11 | Long March 6A | Jun 4, 2026 |
| Qianfan Xingzuo 08 | Long March 6A | May 12, 2026 |
| PRSC-EO3 Mission |
Canonical variants rolled up into this launch vehicle family.
| Variant | Stages | Missions | Status |
|---|---|---|---|
Long March 6 | Not stated | 15 | Active |
Long March 6A | Not stated | 25 | Active |
Long March 6C | Not stated | 1 | Active |
| 2036 | 0 | 16 |
| 2037 | 0 | 16 |
| 2038 | 0 | 16 |
| 2039 | 0 | 16 |
| 2040 | 0 | 16 |
| 2041 | 0 | 16 |
1 launch location represented.
| Year | Location | Launches | Confidence | Basis |
|---|---|---|---|---|
| 2026 | Taiyuan Satellite Launch Center | 10 | 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 | Taiyuan Satellite Launch Center | 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 | Taiyuan Satellite Launch Center | 14 | 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 | Taiyuan Satellite Launch Center | 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... |
| 2030 | Taiyuan Satellite Launch Center | 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... |
| 2031 | Taiyuan Satellite Launch Center | 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... |
| 2032 | Taiyuan Satellite Launch Center | 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... |
| 2033 | Taiyuan Satellite Launch Center | 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... |
| 2034 | Taiyuan Satellite Launch Center | 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... |
| 2035 | Taiyuan Satellite Launch Center | 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... |
| 2036 | Taiyuan Satellite Launch Center | 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... |
| 2037 | Taiyuan Satellite Launch Center | 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... |
| 2038 | Taiyuan Satellite Launch Center | 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... |
| 2039 | Taiyuan Satellite Launch Center | 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... |
| 2040 | Taiyuan Satellite Launch Center | 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... |
| 2041 | Taiyuan Satellite Launch Center | 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... |
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 6C | LEO | 4,500 kg | Unknown | Unknown | Ed Kyle Space Launch Report CZ-5/6/7/8 summary |
Long March 6A | SSO | 4,500 kg | 700 km | Unknown | CASC / SpaceChina Long March 6A page |
Long March 6C | SSO | 2,400 kg | 500 km | Unknown | CASC / SpaceChina Long March 6C page |
Long March 6C | SSO | 2,000 kg | 700 km | Unknown | CASC / SpaceChina Long March 6C page |
Long March 6 | LEO | 1,500 kg | Unknown | Unknown | Ed Kyle Space Launch Report CZ-5/6/7/8 summary |
Long March 6 | SSO | 1,000 kg | 700 km | Unknown | CASC Long March 6 report |
Long March 6 |
| Apr 25, 2026 |
| WHDW 21 | Long March 6A | Apr 8, 2026 |
| Yaogan 50-02 | Long March 6A | Mar 15, 2026 |
| Yaogan 50-01 | Long March 6A | Jan 13, 2026 |
| WHDW 15 | Long March 6A | Dec 8, 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 second stage of the Long March 6A is powered by a single YF-115 engine, producing 18 tons of thrust.
A Long March 6A lifted off at 1240 UTC from Taiyuan.
The total thrust from the first stage and boosters of the Long March 6A is 736 tons.
The first stage of the Long March 6A is powered by two YF-100 engines, generating a total thrust of approximately 244 tons.
The Long March 6A features a two-and-a-half-stage design.
The Long March 6A is the first new-generation launch vehicle in China to utilize a combination of solid and liquid propellants.
The Long March 6A can carry 4,500 kilograms to a 700-kilometer sun-synchronous orbit.
The Long March 6A was developed by the Shanghai Academy of Spaceflight Technology.
The Long March 6A has a payload capacity of 8,000 kilograms to low Earth orbit.
The September 27th launch was the 17th mission for the Long March 6A.
The fairing of the Long March 6A has a diameter of 4.2 meters.
The first and second stages of the Long March 6A have a diameter of 3.35 meters, while the solid-fueled boosters have a diameter of 2 meters.
The Long March 6A took flight just twenty days after the previous mission that launched three Yaogan satellites.
Long March 6A Y16 launched SatNet LEO Group 11.
Frequent Long March 6A launches are enabled by increased workforce and optimizations from team members.
The Long March 6A carried a batch of GuoWang mega-constellation satellites into low Earth orbit.
Shanghai Academy of Spaceflight Technology has improved documentation and personnel handover processes to support a high-density Long March 6A launch schedule.
A Long March 6A launched from Launch Complex 9A at the Taiyuan Satellite Launch Center at 00:34 China Standard Time on September 7, 2025.
Launch teams supporting Long March 6A missions have implemented and refined parallel operations where the next vehicle begins technical preparations at processing facilities before the prior mission launches.
The Long March 6A fairing for the Yaogan-40 Group-03 mission was split into three segments with the uppermost fairing half segment deploying as standard during ascent while the remaining segments stayed attached and were later detached during the deployment sequence.