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SELENE

Former Japanese lunar orbiter spacecraft. SELENE was launched on September 14, 2007 aboard a H-IIA 2022 from Tanegashima. Latest status in GCAT: left Earth orbit for deep space (Sep 14, 2007).

COSPAR 2007-039ANORAD 32054Japan

Identity

Name in GCAT
Kaguya
Common name
SELENE
Payload designation
SELENE
International designator
2007-039A
NORAD catalog number
32054
GCAT identifier
S32054
UN registration
ST/SG/SER.E/533

Mission

Mission type
Deep space
Use
Civil government
Program
JAXA Plan
Owner
JAXA
Country
Japan
Builder
NEC Toshiba Space, Fuchu works
Platform (bus)
SELENE

Launch

Date
September 14, 2007 · 01:31 UTC
Launch record
2007-039Success
Spaceport
Tanegashima · pad Y

Orbit and fate

Orbit class (GCAT)
DSO
Perigee
282 km
Apogee
231,910 km
Inclination
29.90°
Status
Left Earth orbit for deep space
Status date
September 14, 2007
Last known active
Jun 10, 2009
End of operations
Jun 10, 2009

Size

Mass
2,885 kg
Dry mass
1,720 kg
Length
4.7 m
Diameter
2.10 m
Span
30.0 m

Deep space

Deep-space catalog entry
D00860
Final central body
Luna
Phase start
October 3, 2007
Phase outcome
Entered orbit around the target · October 3, 2007
Destination
Luna

Flight phases

FromCentral bodyEndedOutcomeNext
Sep 14, 2007EarthOct 3, 2007Escaped to another bodyLuna
Oct 3, 2007LunaJun 10, 2009DeorbitedLuna

Landings and impacts

WorldTypeResultTouchdownSiteCoordinates
LunaOrbiterTargeted impactJun 10, 2009—-65.50, 80.40

Source: GCAT payload, deep-space and lander catalogs, Jonathan C. McDowell (CC BY 4.0); Wikidata Q205408 (CC0).