Ceres-2

Ceres-2
ManufacturerGalactic Energy
Country of originChina
Size
Diameter3.35 m (11.0 ft)
Stages4
Capacity
Payload to Low Earth orbit
Mass1,600 kg (3,500 lb) (500 km LEO)
Associated rockets
Comparablekuaizhou-11, Jielong 3, Lijian-1
Launch history
StatusActive
Launch sitesJSLC
Total launches2
Success(es)1
Failure1
First flight17 January 2026
Last flight6 November 2026
First stage
Powered by1 Solid
PropellantSolid
Second stage
Powered by1 Solid
PropellantSolid
Third stage
Powered by1 Solid
PropellantSolid
Fourth stage – Advanced liquid upper stage

Ceres-2 (Chinese: 谷神星二号; pinyin: Gǔshénxīng Er-hào; lit. 'Ceres-2'), is a four-stage rocket manufactured and operated by Galactic Energy, the first three stages use solid-propellant rocket motors and the final stage uses a hydrazine propulsion system. The rocket has a diameter of 3.35 metres and it can deliver 1,600 kg (880 lb) to a 500 km low Earth orbit, or 1,300 kg to a 500 km Sun-synchronous orbit. Ceres-2 is a development from the earlier and smaller Ceres-1 launcher.

The first launch of Ceres-2 on 17 January 2026 failed to reach orbit; however the second launch on 6 November 2026 was successful.


Launch statistics summary

0.5
1
1.5
2
2026
'27
'28
  •   Failure
  •   Partial failure
  •   Success
  •   Planned

Launches

References

  1. ↑ Gunter Krebs. "Ceres 2". nextspaceflight.com. Retrieved 6 November 2026.
  2. ↑ Andrew Jones (2 January 2025). "China to debut new Long March and commercial rockets in 2025". SpaceNews.com. Retrieved 6 November 2026.
  3. 1 2 李, 国利; 崔, 婉莹 (6 November 2026). "谷神星二号遥三运载火箭发射成功". XINHUAnet.com. Retrieved 6 November 2026.