长征十号
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 |
|---|---|---|
| 2026 | 1 | 4 |
| 2027 | 0 | 4 |
| 2028 | 0 | 6 |
| 2029 | 0 | 8 |
| 2030 | 0 | 10 |
| 2031 | 0 | 10 |
| 2032 | 0 | 10 |
| 2033 | 0 | 12 |
| 2034 | 0 | 12 |
| 2035 | 0 | 12 |
| 2036 | 0 | 12 |
| 2037 | 0 | 12 |
| 2038 | 0 | 12 |
| 2039 | 0 | 12 |
| 2040 | 0 | 12 |
| 2041 | 0 | 12 |
Payload capacity by variant and target orbit when structured capacity rows are available.
| Variant | Orbit | Capacity | Altitude | Inclination | Source |
|---|---|---|---|---|---|
Long March 10 | LEO | 70,000 kg | Unknown | Unknown | GlobalSecurity CZ-10 |
Long March 10 | TLI | 27,000 kg | Unknown | Unknown | China State Council Long March 10 |
Latest launched missions using variants in this family.
| Mission | Variant | Launch |
|---|---|---|
| CX-26 Mission | Long March 10B | Jul 10, 2026 |
Upcoming mission rows with announced launch timing.
| Mission | Variant | Announced |
|---|---|---|
No forecasted missionsNo upcoming announced mission rows are linked to this vehicle family. | ||
Canonical variants rolled up into this launch vehicle family.
| Variant | Stages | Missions | Status |
|---|---|---|---|
Long March 10 | Not stated | 0 | Development |
Long March 10A | Not stated | 0 | Development |
Long March 10B | 2 | 1 | Active |
1 launch location represented.
| Year | Location | Launches | Confidence | Basis |
|---|---|---|---|---|
| 2026 | Wenchang Space Launch Site | 4 | 20% | Chinese development heavy-launch variant; low-confidence default below mature Long March family rates. |
| 2027 | Wenchang Space Launch Site | 4 | 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 | 6 | 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 | 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... |
| 2030 | Wenchang Space Launch Site | 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... |
| 2031 | Wenchang Space Launch Site | 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... |
| 2032 | Wenchang Space Launch Site | 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... |
| 2033 | 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... |
| 2034 | 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... |
| 2035 | 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... |
| 2036 | 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... |
| 2037 | 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... |
| 2038 | 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... |
| 2039 | 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... |
| 2040 | 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... |
| 2041 | 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... |
Chinese development heavy-launch variant; low-confidence default below mature Long March family rates.
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...
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 10B | LEO | 16,000 kg | Unknown | Unknown | RocketLaunch.org Long March 10B |
Long March 10A | LEO | 14,000 kg | Unknown | Unknown | China State Council Long March 10 Derivative |
China is developing its Long March 10 superheavy rocket, Lanyue lunar lander, and a spacesuit for lunar missions.
The Long March 10A rockets will carry China's next-generation human spacecraft Mengzhou for Earth orbit missions.
To send humans to the Moon, China plans to combine three Long March 10A first stages for the core stage of the Long March 10.
The second Long March 10A booster test fire lasted 320 seconds, longer than the initial test.
On September 12, the China Manned Space Agency conducted multiple test fires for the Long March 10 series of crew-capable rockets.
The Long March 10 manned space launch vehicle has completed a successful second firing test.
The successful second firing test marks a breakthrough in the development of the Long March 10 vehicle.
Tethered firing tests for the Long March 10 vehicle were completed as planned at the Wenchang Space Launch Site.
The second static fire test of Long March 10 focused on engine throttling and reignition.
Both Long March 10 series rockets, the Long March 10A2 and Long March 103, are preparing for their debut flights in 2026 and early 2027.
The Long March 10 series rocket can lift up to 18,000 kilograms into low Earth orbit.
The recovery phase operating procedure design for the Long March 10 series was verified as correct and reliable.
The tethered ignition tests of the Long March 10 series are conducted step-by-step for performance verification and recovery reuse objectives.
The Long March 10 series rocket is capable of sending up to 27,000 kilograms on a trans-lunar trajectory.
The two planned tethered ignition tests for the Long March 10 series have been completed, confirming the performance of the rocket's first-stage power system.
A second static fire test of Long March 10 was completed on September 12.
The China Academy of Launch Vehicle Technology and the China Manned Space Agency conducted a static fire test for the Long March 10 series on September 12th at 15:00 China Standard Time.
A static fire test for the 2nd CZ-10 is planned for tomorrow, the 12th.
On August 15, the China Manned Space Agency and the China Academy of Launch Vehicle Technology conducted a 30-second static fire test for the Long March 10 series of crew-capable rockets.
The Long March 10A rockets will launch China's next-generation human spacecraft named Mengzhou to Earth orbit.