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 Long March 6A fairing has a diameter of 4.2 meters.
The Long March 6A weighs 530,000 kilograms when fully fueled.
The Long March 6A second stage is powered by a single YF-115 engine producing 18 tons of thrust.
Yaogan 50-02 reached orbit after a successful Long March 6A launch at 13:22 UTC on March 15, 2026.
The Long March 6A launch was scheduled for 1:24 PM UTC.
The March 15 mission was the 21st launch of the Long March 6A.
The launch vehicle was a Long March 6A.
The Long March 6A is used to deploy Chinese low-Earth-orbit communications satellites and other satellite constellations.
The Long March 6A has a payload capacity of 8,000 kilograms to low Earth orbit.
The Long March 6A boosters generate a combined thrust of 492 tons.
The Long March 6A solid-fueled boosters have a diameter of 2 meters.
The Long March 6A was developed by the Shanghai Academy of Spaceflight Technology.
The Long March 6A has flown 12 missions since January 2025.
The Long March 6A first stage is augmented by four solid rocket boosters that each produce 124 tons of thrust.
The Long March 6A is the first new-generation Chinese launch vehicle to use a combination of solid and liquid propellants.
The Long March 6A first stage is powered by two YF-100 engines with a combined thrust of approximately 244 tons.
The Long March 6A uses a two-and-a-half-stage design.
A larger GuoWang satellite platform roughly 30 percent bigger and weighing up to 1,000 kilograms is launched via Long March 5B and Long March 6A.
LeoLabs found a median radar cross section (RCS) of 6.2 square meters for GuoWang satellites launched by Long March 6A.
LeoLabs analysis indicates near-polar GuoWang groups launched by Long March 6A and Long March 5B are probably using the larger satellite platform while groups launched by Long March 8A and Long March 12 are probably using the smaller platform.