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APOLLO 10 LM APS

activeHuman SpaceflightHeliocentric

The S-IVB was the third stage on the Saturn V and second stage on the Saturn IB launch vehicles. Built by the Douglas Aircraft Company, it had one J-2 rocket engine. For lunar missions it was fired twice: first for Earth orbit insertion after second stage cutoff, and then for translunar injection (TLI).

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Launch

Launch date
May 18, 1969 at 04:49 PM UTC
Launch site
Cape Canaveral SFS, USA
Launched by
Saturn V →
Operator
National Aeronautics and Space Administration
Mission
Apollo 10
Launch record
View full launch →

Trajectory

Regime
Interplanetary — Heliocentric
Reference body
Heliocentric

Identity

COSPAR (Int'l)
1969-043D
NORAD catalog №
3949
Object type
Payload
Owner / operator
United StatesUnited States
Status
active