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 2F is 62 meters tall and weighs 464,000 kilograms when fully fueled.
The launch of the Long March 2F series is the 26th, and the 604th launch of the Long March vehicle series.
The first-stage of the Long March 2F is powered by four YF-20B engines generating a combined thrust of 332 tons.
The Long March 2F/G has a payload capacity of 8,400 kilograms to low Earth orbit.
The Shenzhou spacecraft launches on the Long March 2F/G rocket from the Jiuquan Satellite Launch Center.
Planned tests, team drills, and launch rehearsals were completed before the Long March 2F/G's rollout to the launch pad on October 24th.
The three astronauts will be launched from the Jiuquan Satellite Launch Center at 11:44 PM local time on October 31 on a Long March 2F rocket.
A Long March 2F/G lifted off from Launch Area 4 at the Jiuquan Satellite Launch Center on October 31st, carrying a Shenzhou spacecraft with three taikonauts onboard into low Earth orbit.
The Long March 2F is the only human-rated launch vehicle currently active in China, developed by the China Academy of Launch Vehicle Technology.
The total combined thrust of the first-stage and four boosters of the Long March 2F is 664 tons.
The Long March 2F/G launch vehicle is designed to send the Shenzhou spacecraft onto a rendezvous path with the Tiangong Space Station in three and a half hours.
The Shenzhou spacecraft currently launches on the Long March 2F/G rocket.
Zenkspace's offering is expected to outperform the CZ-2/4 series.
The CZ-2F/G, also known as the Long March 2F/G, is 62 m tall and 3.35 m in diameter.
The spacecraft is mated with a Long March 2F carrier rocket and has been transferred to the launch area.
Pre-launch checks are underway for the Shenzhou-21 spacecraft and Long March-2F Y21 rocket.
The Long March-2F Y21 rocket is ready for launch.
The second stage of the Long March 2F is powered by one YF-24B engine generating 85 tons of thrust.
The Long March 2F/G launches the Shenzhou spacecraft, while the 2F/T launches China’s reusable spaceplane and the first two Tiangong space stations.
The total thrust of the first stage along with the four boosters of the Long March 2F is 664 tons.