For the Apollo 16 Saturn booster that impacted the Moon, from the Apollo 16 Saturn V launch vehicle report AS-511, pg 17-5 (lunar impact section).... Geocentric Orbit Parameters following APS Impact Burn Semimajor Axis 232057 km Eccentricity .971884 C3, km^2/s^2 -1.717695 (twice the specific energy of the orbit) Perigee Radius 6525 km Range Time 20461.4 seconds GMT Time, 16 April, 22hr:12 min:07 sec= Range time 4 hr:18min:7 sec.(15487sec) Other stuff available if useful. ------------------------------------------------------------------------- Subscribe/Unsubscribe info, Frequently Asked Questions, SeeSat-L archive: http://www.satobs.org/seesat/seesatindex.html
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