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.
A Long March 2F/T launch vehicle lifted off from Launch Site 91 at the Jiuquan Satellite Launch Center between 11:48 am and 12:07 pm China Standard Time (03:45 and 04:07 am UTC) on February 7th.
Two versions of the Long March 2F are currently active: the 2F/G and the 2F/T.
The Long March 2F boosters have a diameter of 2.3 meters each.
The launch on February 7, 2026 used a Long March-2F carrier rocket.
With the February 7th launch, the Jiuquan Satellite Launch Center’s Long March 2F series facilities can shift to solely working on upcoming crewed missions.
The China Academy of Launch Vehicle Technology developed the Long March 2F.
The February 7th launch was the 28th launch of the Long March 2F series.
A Long March 2F rocket lifted off from the Jiuquan Satellite Launch Center carrying a classified Reusable Experimental Spacecraft into orbit.
The Long March 2F first and second stages have a diameter of 3.35 meters.
The Long March 2F/T launch vehicle carried China’s Reusable Experimental Spacecraft into low Earth orbit on February 7th.
The Long March 2F/T launches China’s reusable spaceplane and launched the first two Tiangong space stations.
The four boosters of the Long March 2F are each powered by one YF-20B engine producing 83 tons of thrust each for a combined booster thrust of 332 tons and burning dinitrogen tetroxide and unsymmetrical dimethylhydrazine.
The Long March 2F is the only human-rated launch vehicle currently active in China.
The Shenzhou spacecraft protective fairing used with the Long March 2F has a maximum diameter of 3.6 meters.
The Long March 2F/G launches the Shenzhou spacecraft.
The combined thrust of the Long March 2F first stage and four boosters is 664 tons.
A Long March 2F (CZ-2F) rocket launched from Jiuquan at about 03:57 UTC on February 7, 2026.
The fully fueled launch mass of the Long March 2F is 464,000 kilograms.
The Long March 2F payload capacity is 8,600 kilograms to low Earth orbit with a 4.2-meter-wide fairing.
The first stage of the Long March 2F is powered by four YF-20B engines producing a combined 332 tons of thrust and burning dinitrogen tetroxide and unsymmetrical dimethylhydrazine.