Navstar 65

 2012-053A

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Block IIF SV-4?/ SVN 65 / PRN 24 Replaces 2A21/SV39/PRN09 in plane A1 The Delta second stage suffered a fuel leak which resulted in engine thrust reaching only 95 percent of the planned value in all three of its burns, but the automated vehicle compensated, and had enough margin that the correct orbit was reached using slightly longer burn times.

GPS 65
Date	Time	Event	Orbit
2012 Oct 4	1210:00	Launch by Delta 4M+(4,2)	CC SLC37B
		T+1:34 GEM60 SRM burnout
		T+1:40 SRM sep
		T+4:05 MECO
		T+4:11 CBC sep
	1214:26	T+4:26 Stage 2 SES-1
		T+4:36 Payload fairing
	1212:11	T+12:11 SECO-1	163 x 394 x 41.6
	1231:17	T+21:17 SES-2
	1234:34	T+24:34 SECO-2	239 x 20374 x 43.3
	1530:44	T+3:20:44 SES-3
	1532:22	T+3:22:22 SECO-3	20459 x 20459 x 55
		T+3:28:53 Spinup
	1543:03	T+3:33:03 GPS sep from Delta