Mission record
Chang'e 6
Also known as Chang'e-6
China National Space Administration · Launched
Explore trajectoryCompleted · Success
China's Chang'e 6 returned the first samples from the lunar far side after landing in the South Pole-Aitken Basin.
- Destinations
- Launch vehicle
- Long March 5
- Launch site
- Wenchang Space Launch Site
- Countries
- China
- Mission types
- Lander, Sample return
Chronology
Mission timeline
Launch
Chang'e 6 launched on a Long March 5 from Wenchang Space Launch Site
Original China standard time (UTC+08:00) converted to UTC at the published minute precision.
EarthOrbit insertion
Chang'e 6 entered circumlunar orbit
10:12 China standard time converted to UTC at the published minute precision.
MoonLanding
Chang'e 6 landed in the South Pole-Aitken Basin
Original China standard time (UTC+08:00) converted to UTC at the published minute precision.
MoonDeparture
Chang'e 6 ascender lifted off from the lunar surface with far-side samples
Original China standard time (UTC+08:00) converted to UTC at the published minute precision.
MoonMilestone
Chang'e 6 ascender transferred far-side samples to the returner in lunar orbit
Original China standard time (UTC+08:00) converted to UTC at the published minute precision.
MoonSample return
Chang'e 6 returner brought the first lunar far-side samples back to Earth
Original China standard time (UTC+08:00) converted to UTC at the published minute precision.
EarthDeployment
The lander and ascender separated from the orbiter and returner
CNSA reports May30 China standard time without a clock. The corresponding possible UTC interval is May29 16:00 through May30 16:00 (exclusive); a unique UTC calendar day or separation instant is not established.
Milestone
The autonomous mobile camera photographed the lander and ascender on June3 China time
The primary report supplies a local calendar day without a clock. Do not manufacture an exact UTC release or imaging time.
Mission architecture
Vehicles
Chang'e 6 orbiter · Orbiter · Carried the return capsule; continued independently after capsule release. Extended flight coverage is reviewed separately.
Destinations: Moon
Chang'e 6 lander · Lander
Destinations: Moon
Chang'e 6 ascender · Spacecraft · Carried on the lander, then independently launched from the Moon and docked in lunar orbit.
Destinations: Moon
Chang'e 6 autonomous mobile camera · Rover · Approximately 5 kg autonomous robot released after sampling; independently moved to photograph the lander and ascender. No dated traverse yet acquired.
Destinations: Moon
Chang'e 6 return capsule · Return capsule · Recovered on Earth after sample transfer and release from the orbiter.
Destinations: Moon
Trajectory record
Time-dependent navigation trajectory
Source states place the model at the selected time. Reconstructed flight, estimates, predictions and historical mission plans are identified by interval; gaps remain visible.
Source records and sampling assumptions are retained with the repository data. Model attitude and surface appearance are illustrative.
- Chang'e 6 orbiter and attached returner: Project Pluto optical-fit Chang'e 6 return-stack estimate, 22–23 June 2024 before the reported maneuver; other phases uncovered. · June 22, 2024 to June 23, 2024
Provenance
Sources
Each source is listed once and labeled with the mission, event, trajectory, or destination/body context it supports.
Data verified through October 11, 2026
- Robotic probe launched to lunar far side - CNSA — CNSAOther · Supports: mission claims
- China's Chang'e-6 lands on moon's far side to collect samples - CNSA — CNSAOther · Supports: mission claims
- About China's lunar mission: Timeline of Chang'e-6 mission - CNSA — CNSAOther · Supports: mission claims · event claims
- NASA’s LRO Spots China’s Chang'e 6 Spacecraft on Lunar Far Side - NASA — NASAOther · Supports: mission claims
- Chang'e-6 autonomous mobile camera: actual deployment and imaging — CNSATechnical document · Supports: mission claims · event claims
- GRAS Chinese lunar exploration science catalog and original product descriptions — OTHERTechnical document · Supports: mission claims
- CAST: original four-component Chang’e-5 design and separation systems — OTHERTechnical document · Supports: mission claims
- CAS: Chang’e-5 T1 service bus and return-capsule description — OTHERTechnical document · Supports: mission claims
- CNSA / CAST: Chang’e-6 actual landing and deployment design — CNSATechnical document · Supports: mission claims · event claims
- CNSA: Chang’e-6 sample collection and ascent — CNSATechnical document · Supports: mission claims · event claims
- CNSA: Chang’e-6 docking and sample transfer — CNSATechnical document · Supports: mission claims · event claims
- CNSA: Chang’e-6 separation sequence, atmospheric entry and recovery — CNSATechnical document · Supports: mission claims · event claims
- CNSA: Chang’e-6 flight retrospective — CNSATechnical document · Supports: mission claims · event claims
- CNSA: Chang’e-6 lunar capture — CNSATechnical document · Supports: mission claims · event claims
- Yan et al.: Microtopography of the Chang’e-6 landing area revealed by photogrammetry, original maps and camera images — OTHERTechnical document · Supports: mission claims
- CNSA: Chang’e-6 chief designer explains the autonomous mobile camera — CNSATechnical document · Supports: mission claims
- Chang'e 6 Project Pluto optical orbit fit — OTHERArchive · Supports: mission claims
- DE421 lunar mean-Earth and principal-axes frame specification — NAIFTechnical document · Supports: destination/body context
- DE440 lunar mean-Earth and principal-axes frame specification — NAIFSpice · Supports: destination/body context
- IAU rotational elements and body radii (PCK 00011) — NAIFSpice · Supports: destination/body context
- LOLA global lunar height maps, LDEM_4 V3 original PDS source label — NASATechnical document · Supports: destination/body context
- LOLA 2023 south-polar elevation, uncertainty and effective-resolution maps — NASATechnical document · Supports: destination/body context
- Blue Ghost Lunar Lander Seen From Above: LROC site and terrain context — NASATechnical document · Supports: destination/body context
- Moon Facts — NASAOther · Supports: destination/body context
- SLDEM2015 Blue Ghost region: original PDS elevation-grid label — NASATechnical document · Supports: destination/body context
- JPL Solar System Dynamics Astrodynamic Parameters — JPLOther · Supports: destination/body context
- Planet Sizes and Locations in Our Solar System — NASAOther · Supports: destination/body context