Launch success.
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Historical mission record
This page records Zhuque-2E | Guangchuan-01 & 02 and its reported outcome: Launch Successful. The date above is a historical record.
Source record updated . This is a source update, not a confirmed launch time.
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What changed?
Added launch per NOTAMs; Launch vehicle and payload identities uncertain.
Update ↗Status reported by the mission data provider.
Mission
2 satellites for testing and demonstrating LEO communication satellite constellation technologies. First flight of the enhanced Zhuque-2.
- Launch vehicle
- Zhuque-2E
- Mission type
- Technology
- Destination orbit
- Low Earth Orbit
- Launch pad
- Launch Area 96A
- Provider
- LandSpace
The vehicle
Published configuration and flight history.

Zhuque-2E
Zhuque-2E (E stands for “enhanced”) is a medium-sized rocket powered by liquid oxygen and methane capable of lifting 6,000 kg of payload into a 200 km low Earth orbit, or 4,000 kg of payload into a 500 km Sun-synchronous orbit. It differs from the baseline Zhuque-2 in using enhanced TQ-12A engines on the 1st stage with higher thrust and specific impulse than the original TQ-12, and a new TQ-15A engine on the 2nd stage that has a moveable nozzle.
- Height
- 49.5 m
- Diameter
- 3.35 m
- Stages
- 2
- Recorded launches
- 3
- First flight
- 2024-11-27
Recorded timing
This is a mission record, not an upcoming calendar appointment.
Target ·
The target marker shows its position within the published window. The schedule may change before launch.
Launch site & orbit
Jiuquan Satellite Launch Center, People's Republic of China
Launch site & orbit
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Coverage & sources
Links supplied by the mission data provider.
Coverage and times may change.
Mission coverage
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Further reading
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