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Chang'e 2

Chinese Moon orbiter. Chang'e 2 was launched on October 1, 2010 aboard a Chang Zheng 3C from Xichang. Latest status in GCAT: left Earth orbit for deep space (Oct 2, 2010).

COSPAR 2010-050ANORAD 37174China

Identity

Name in GCAT
Chang'e-2
Common name
Chang'e 2
Other names
CE-2
International designator
2010-050A
NORAD catalog number
37174
GCAT identifier
S37174
UN registration
ST/SG/SER.E/649

Mission

Mission type
Deep space
Use
Civil government
Program
Chang'e
Owner
CASC
Country
China
Builder
Chinese Academy of Space Technology, Beijing (CASC 5th Acad)
Platform (bus)
DFH-3

Launch

Date
October 1, 2010 · 10:59 UTC
Launch record
2010-050Success
Spaceport
Xichang · pad LC2

Orbit and fate

Orbit class (GCAT)
CLO
Perigee
300 km
Apogee
380,000 km
Inclination
32.40°
Status
Left Earth orbit for deep space
Status date
October 2, 2010
Last known active
2014
End of operations
December 2012

Size

Mass
2,480 kg
Dry mass
1,000 kg
Length
2.2 m
Diameter
1.70 m
Span
18.0 m

Deep space

Deep-space catalog entry
D00902
Final central body
Luna
Phase start
October 5, 2010
Phase outcome
Entered orbit around the target · October 6, 2010
Destination
Luna

Flight phases

FromCentral bodyEndedOutcomeNext
Oct 2, 2010EarthOct 5, 2010Escaped to another bodyLuna
Oct 6, 2010LunaJun 9, 2011Left orbit around the targetLuna
Jun 9, 2011LunaJun 9, 2011Escaped to another bodyEarth
Jun 9, 2011EarthAug 25, 2011Escaped to another bodySEL2
Aug 25, 2011SEL2May 30, 2012Escaped to another bodyHCO
Dec 13, 2012ToutatisDec 13, 2012FlybyHCO

Source: GCAT payload, deep-space and lander catalogs, Jonathan C. McDowell (CC BY 4.0); Wikidata Q831345 (CC0).