Key facts
- Mission type
- Lunar orbiter, Asteroid flyby, Technology demonstration
- Operator
- CNSA
- Cospar id
- 2010-050A
- Mission duration
- Planned: 6 months , Final: ~4 years
- Bus
- DFH-3
- Launch mass
- 2,480 kg
- Launch date
- 1 October 2010, 10:59 ( 2010-10-01UTC10:59Z ) UTC
- Rocket
- Chang Zheng 3C
- Launch site
- Xichang LC-2
- Reference system
- Heliocentric
- Orbital insertion
- 6 October 2010, 03:06 UTC
- Orbital departure
- 8 June 2011
- Closest approach
- 13 December 2012, 08:30 UTC
- Distance
- 3.2 kilometres (2.0 mi)
via Wikipedia infobox
Wikidata facts
- Instance of
- artificial satellite
- Named after
- Chang'e
- Followed by
- Chang'e 3
- Follows
- Chang'e 1
- Mass
- 2480
- Significant event
- rocket launch
Show 5 more facts
- UTC date of spacecraft launch
- 2010-10-01
- space launch vehicle
- Long March 3C
- start point
- Xichang Satellite Launch Center
- type of orbit
- lunar orbit
- Commons category
- Chang'e 2
Sources (1)
via Wikidata · CC0