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...
GuoWang large satellite platforms’ mass could be between 700 kilograms and 1,000 kilograms based on Long March 6A and Long March 5B sun-synchronous payload capacity considerations and an approximately 8,000-kilogram Yuanzheng-2 upper stage.
The Long March 6A is the only GuoWang launcher to use a 4.2-meter-diameter fairing and has delivered five GuoWang spacecraft into orbit per launch.
Two different satellite variants are believed to be in use for the GuoWang constellation, with a larger variant launched on vehicles like the Long March 5B and smaller variants launched on rockets such as the Long March 12 and Long March 6A.
The Long March-6A carried the Yaogan-50 01 satellite.
China successfully launched the Long March-6A at 22:16 on January 13.
The Long March 6A is approximately 52 meters tall and weighs 530,000 kilograms when fully fueled.
The GuoWang constellation includes two satellite variants, with larger ones launched on vehicles like the Long March 5B and smaller ones on the Long March 12 or Long March 6A.
Insulative materials were installed on the Long March 6A, and heaters were used to keep critical systems warm.
The total thrust generated by the first stage and solid rocket boosters of the Long March 6A is 736 tons.
The Long March 6A successfully launched the Yaogan 50-01 satellite.
The Long March 6A launched at 22:16 pm China Standard Time carrying the Yaogan-50-01 remote sensing satellite.
All Long March 6A launches have taken place at the Taiyuan Satellite Launch Center in Shanxi province.
Today's launch was the 20th mission for the Long March 6A and the first launch from China in 2026.
The diameter of the fairing on the Long March 6A is 4.2 meters.
China's Long March 6A launched from Launch Complex 9A at the Taiyuan Satellite Launch Center on January 13th, 2026.
The second stage of the Long March 6A is powered by a single YF-115 engine producing 18 tons of thrust.
The first stage of the Long March 6A has four solid rocket boosters, each producing 124 tons of thrust, resulting in a total booster thrust of 492 tons.
The diameter of the first and second stages of the Long March 6A is 3.35 meters, while the solid-fueled boosters have a diameter of 2 meters.
The Long March 6A is powered by two YF-100 engines producing a combined thrust of approximately 244 tons.
Long March 6A Y27 launched the Yaogan-50-01 satellite.