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   ocr: Apollo 13 Mission Events GET Vel. Change Events Hra.:Min. Date/EST Feet/Bec. Purpose & Resultant Orbit Eerth orbit insertion 00:11 11 2:24 p.m. 25,593 Insertion into 103 nu cir- cular Rarth parking orbit, Tranelunar injection 02:35 11 4:48 p.m, 10,437. Injection into free-return (8-IVB Engine ignition) transiunar trajectory with 210 mo pericynthion. CSM Beparation, docking 03:06 11 - 5:19 p.m, - Hard-mating of CSI and LM Ejection from SLA 04:00 11 6:14 p.. 1 separates CSM-LM frou S-1VB-SHA. S-IVB evasive maneuver 04:19 I1 6:32 p.0. 9,4 Provides separation prior to S-IVB propellant dump and thr ...