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Apollo 6 Lunar Module test article

Modified Lunar Module for Apollo 6. Apollo 6 Lunar Module test article was launched on April 4, 1968 aboard a Saturn V from Cape Canaveral & Kennedy. Latest status in GCAT: reentered (orbital decay) (Sep 3, 1968).

COSPAR 1968-025ENORAD 3187United States

Identity

Name in GCAT
LTA-2R
Common name
Apollo 6 Lunar Module test article
International designator
1968-025E
NORAD catalog number
3187
GCAT identifier
S03187

Mission

Mission type
Human spaceflight
Use
Civil government
Program
LTA
Owner
MSC
Country
United States
Builder
Grummann Aerospace Corporation
Platform (bus)
LTA

Launch

Date
April 4, 1968 · 12:00 UTC
Launch record
1968-025Success
Rocket
Saturn V
Spaceport
Cape Canaveral & Kennedy · pad LC39A

Orbit and fate

Orbit class (GCAT)
LLEO/I
Perigee
236 km
Apogee
359 km
Inclination
32.57°
Status
Reentered (orbital decay)
Status date
September 3, 1968
Last known active
Apr 4, 1968
End of operations
Apr 4, 1968

Size

Mass
11.8 t
Dry mass
11.8 t
Length
7.0 m
Diameter
4.30 m
Span
7.0 m

Source: GCAT payload, deep-space and lander catalogs, Jonathan C. McDowell (CC BY 4.0); Wikidata Q89642682 (CC0).