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 spacecraft launched on the Long March 6A and Long March 5B use a large satellite platform with a mass of at most 1,000 kilograms.
The Long March 6A has a payload capacity of 8,000 kilograms to low Earth orbit.
The Long March 6A launch of SatNet LEO Group 21 was scheduled for 7:37 PM UTC.
The launch was the 22nd mission for the Long March 6A.
All Long March 6A launches have taken place from the Taiyuan Satellite Launch Center in Shanxi province.
The Long March 6A is up to 52 meters tall and weighs 530,000 kilograms when fully fueled.
The Long March 6A was developed by the Shanghai Academy of Spaceflight Technology.
SatNet LEO Group 21 launched on a Long March 6A rocket from Taiyuan Satellite Launch Center in China.
The Long March 6A has a payload capacity of 4,500 kilograms to a 700-kilometer sun-synchronous orbit.
Yaogan-50-02 departed the Taiyuan Satellite Launch Center atop a Long March 6A rocket.
A Long March 6A launched from Taiyuan at 1322 UTC on March 15, 2026 carrying the Yaogan-50 (02) satellite.
The Long March 6A launch placed Yaogan-50-02 into a retrograde low Earth orbit with a single satellite.
The Long March 6A has a payload capacity of 4,500 kilograms to a 700-kilometer sun-synchronous orbit.
The Long March 6A has flown 21 missions since its debut four years ago.
The Long March 6A is believed to be up to 52 meters tall.
The Long March 6A first and second stages have a diameter of 3.35 meters.
Every Long March 6A launch to date has taken place from the Taiyuan Satellite Launch Center in Shanxi province.
A Long March 6A launched from Launch Complex 9A at the Taiyuan Satellite Launch Center on March 15 at 21:22 China Standard Time and 13:22 Universal Coordinated Time.
Long March 6A Y28 launched Yaogan-50-02 from Taiyuan on March 15, 2026.
The Long March 6A first stage and boosters generate a total thrust of 736 tons.