长征二号
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 | 2 | 0 |
| 2020 | 11 | 0 |
| 2021 | 14 | 0 |
| 2022 | 24 | 0 |
| 2023 | 25 | 0 |
| 2024 | 18 | 0 |
| 2025 | 13 | 0 |
| 2026 | 9 | 8 |
| 2027 | 0 | 8 |
| 2028 | 0 | 8 |
| 2029 | 0 | 8 |
| 2030 | 0 | 8 |
| 2031 | 0 | 8 |
| 2032 | 0 | 8 |
| 2033 | 0 | 8 |
| 2034 | 0 | 8 |
| 2035 | 0 | 8 |
Payload capacity by variant and target orbit when structured capacity rows are available.
| Variant | Orbit | Capacity | Altitude | Inclination | Source |
|---|---|---|---|---|---|
Long March 2F G | LEO | 8,400 kg | Unknown | Unknown | Manual Long March crew-launch vehicle capacity fallback. |
Long March 2F T | LEO | 8,400 kg | Unknown | Unknown | Manual Long March crew-launch vehicle capacity copied from sibling Chang Zheng 2F G row. |
Long March 2C | LEO | 3,850 kg | Unknown | Unknown | RocketLaunch.org Long March 2C vehicle page |
Latest launched missions using variants in this family.
| Mission | Variant | Launch |
|---|---|---|
| WHJSW 10 | Long March 2D | May 30, 2026 |
| Shenzhou 23 Mission | Long March 2F G | May 24, 2026 |
| WHJSW 9-1 to 9-4 | Long March 2D | Apr 24, 2026 |
| Shiyan 33 Mission |
Canonical variants rolled up into this launch vehicle family.
| Variant | Stages | Missions | Status |
|---|---|---|---|
Long March 2 | Not stated | 2 | Retired |
Long March 2C | Not stated | 50 | Active |
Long March 2C a | Not stated | 2 | Retired |
Long March 2C b | Not stated | 26 | Retired |
| 2036 | 0 | 8 |
| 2037 | 0 | 8 |
| 2038 | 0 | 8 |
| 2039 | 0 | 8 |
| 2040 | 0 | 8 |
| 2041 | 0 | 8 |
1 launch location represented.
| Year | Location | Launches | Confidence | Basis |
|---|---|---|---|---|
| 2026 | China inland launch centers | aggregate | 8 | 25% | Editable low-confidence Long March workhorse variant annual throughput default. |
| 2027 | China inland launch centers | aggregate | 8 | 25% | Editable low-confidence Long March workhorse variant annual throughput default. |
| 2028 | China inland launch centers | aggregate | 8 | 25% | Editable low-confidence Long March workhorse variant annual throughput default. |
| 2029 | China inland launch centers | aggregate | 8 | 25% | Editable low-confidence Long March workhorse variant annual throughput default. |
| 2030 | China inland launch centers | aggregate | 8 | 25% | Editable low-confidence Long March workhorse variant annual throughput default. |
| 2031 | China inland launch centers | aggregate | 8 | 25% | Editable low-confidence Long March workhorse variant annual throughput default. |
| 2032 | China inland launch centers | aggregate | 8 | 25% | Editable low-confidence Long March workhorse variant annual throughput default. |
| 2033 | China inland launch centers | aggregate | 8 | 25% | Editable low-confidence Long March workhorse variant annual throughput default. |
| 2034 | China inland launch centers | aggregate | 8 | 25% | Editable low-confidence Long March workhorse variant annual throughput default. |
| 2035 | China inland launch centers | aggregate | 8 | 25% | Editable low-confidence Long March workhorse variant annual throughput default. |
| 2036 | China inland launch centers | aggregate | 8 | 25% | Editable low-confidence Long March workhorse variant annual throughput default. |
| 2037 | China inland launch centers | aggregate | 8 | 25% | Editable low-confidence Long March workhorse variant annual throughput default. |
| 2038 | China inland launch centers | aggregate | 8 | 25% | Editable low-confidence Long March workhorse variant annual throughput default. |
| 2039 | China inland launch centers | aggregate | 8 | 25% | Editable low-confidence Long March workhorse variant annual throughput default. |
| 2040 | China inland launch centers | aggregate | 8 | 25% | Editable low-confidence Long March workhorse variant annual throughput default. |
| 2041 | China inland launch centers | aggregate | 8 | 25% | Editable low-confidence Long March workhorse variant annual throughput default. Site-year coverage backfill copied nearest prior site-rate row. |
Editable low-confidence Long March workhorse variant annual throughput default.
Editable low-confidence Long March workhorse variant annual throughput default.
Editable low-confidence Long March workhorse variant annual throughput default.
Editable low-confidence Long March workhorse variant annual throughput default.
Editable low-confidence Long March workhorse variant annual throughput default.
Editable low-confidence Long March workhorse variant annual throughput default.
Long March 2C | SSO | 2,500 kg | 700 km | Unknown | CASC Long March 2C/YZ-1S launch report |
Long March 2D | SSO | 1,300 kg | 700 km | Unknown | SAST Long March 2D launch report |
Long March 2C | GTO | 1,250 kg | Unknown | Unknown | RocketLaunch.org Long March 2C vehicle page |
Long March 2C |
| Mar 27, 2026 |
| Siwei Gaojing 2-05/06 | Long March 2D | Mar 25, 2026 |
| Shiyan 30 03/04 | Long March 2D | Mar 12, 2026 |
| CSSHQ | Long March 2F T | Feb 7, 2026 |
| Alsat-3B | Long March 2C | Jan 31, 2026 |
Upcoming mission rows with announced launch timing.
| Mission | Variant | Announced |
|---|---|---|
No forecasted missionsNo upcoming announced mission rows are linked to this vehicle family. | ||
Long March 2C-III | Not stated | 7 | Retired |
Long March 2C SM | Not stated | 2 | Retired |
Long March 2C SMA | Not stated | 3 | Retired |
Long March 2D | Not stated | 102 | Active |
Long March 2D a | Not stated | 3 | Retired |
Long March 2E | Not stated | 7 | Retired |
Long March 2F | Not stated | 7 | Retired |
Long March 2F G | Not stated | 16 | Active |
Long March 2F T | Not stated | 6 | Active |
Editable low-confidence Long March workhorse variant annual throughput default.
Editable low-confidence Long March workhorse variant annual throughput default.
Editable low-confidence Long March workhorse variant annual throughput default.
Editable low-confidence Long March workhorse variant annual throughput default.
Editable low-confidence Long March workhorse variant annual throughput default.
Editable low-confidence Long March workhorse variant annual throughput default.
The Long March 2C can deliver 3,850 kilograms to low Earth orbit, 1,900 kilograms to sun-synchronous orbit, and 1,250 kilograms to geostationary transfer orbit.
The launch at Jiuquan SLC had been assigned four different Chinese rockets before being settled on a Long March 2C with a Yuanzheng-1S upper stage.
A Long March 2C rocket with a Yuanzheng-1S upper stage launched successfully at 04:11 UTC on March 27, 2026.
The Long March 2C launch carried a single payload toward sun-synchronous orbit.
The Long March 2C is used for missions to low Earth orbit and sun-synchronous orbit.
The Long March 2C is 42 meters tall and weighs 233,000 kilograms when fully fueled.
This mission was the 87th launch of the Long March 2C.
The Long March 2C first stage uses four YF-21C engines that generate 302 tons of thrust.
A Long March 2D rocket was being stacked for launch on March 26, 2026.
After its latest upgrades, CALT's Long March 2C has about 100 kg more lift capability than SAST's Long March 2D.
A Long March 2C launch vehicle was headed to sun-synchronous orbit.
A mission swapped from CALT's Long March 2C to SAST's Long March 2D.
A Long March 2C rocket with a YZ-1 upper stage lifted off from Jiuquan on March 23, 2026.
The launch is not believed to use a Long March 2 or Long March 4 rocket or an SRB-based launcher.
A Long March 2D rocket marked CZ-2D is at Xichang Satellite Launch Center in China.
The launch vehicle for the Xichang mission on March 12, 2026 is potentially a Long March 2D or the similar Long March 2C.
The Xichang launch vehicle was likely a Long March 2D but could instead be a Long March 2C.
Rong Yi, an Expert Rocket Designer who led development of the Long March 10A while serving as the Long March 2F’s Chief Designer, led the booster’s development.
The Long March 2F payload capacity is 8,400 kilograms to low Earth orbit with Shenzhou’s abort systems.
The Long March 2F second stage is powered by one YF-24B engine generating 85 tons of thrust and burning dinitrogen tetroxide and unsymmetrical dimethylhydrazine.