For Apollos 8, 10, 11 and 12, the excess LOX on the S-IVB was vented in a forward direction to slow the stage down. This allowed the moon to cross its path before it got there, so it swung around the trailing "edge" of the moon. The moon dragged it along in its orbit, acting as a slingshot to eject it into an earth escape trajectory so that they went into independent orbits around the sun -- where they remain today.
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For the early missions that used the free-return trajectory, they almost certainly looped around the moon, returned to earth and hit the atmosphere. I'm not sure about the later missions, but they're likely in solar orbit.
I don't mean to derail the thread, but there has to be a way to calculate exactly where these things are today, isn't there?
I mean, if the velocities, attitude, inclination, and locations of all of the spacecraft were known when the stagings occurred, (and at the time, they had to be, didn't they?) then someone who knows what they're doing should be able to calculate the physical location in orbit of these pieces of hardware.
If JPL could calculate where Pluto was going to be 9 years before the launch of New Horizons, and only miss it by 7 seconds, and its 3.8 billion miles away, then the positions of the Apollo stages ought to be able to be calculated.
It would be nice if something like this were in Stellarium or something. I don't know if my 'scope could resolve something that small, and I don't think it could, but it would be pretty cool to know where to look.