Los Angeles: August 2012

 https://welib.org/md5/8f6bc918e82e4ef7f7466de1c7d7d3ee

Beidou 11

 2010-068A

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di qi ke beidou daohang weixing, 7th Beidou navsat.

China launched the 7th Beidou Navigation Satellite (di qi ke beidou daohang weixing) on Dec 17 from the Xichang Satellite Launch Center (xichang weixing fashe zhongxin). The launch vehicle was the "Changzheng sanhao jia" (Long March 3A).

It was the second satellite in the series to be sent to inclined geosynchronous orbit.

BDW7
Date	Time	Event	Orbit
2010 Dec 17	2020:04	Launch by CZ-3A	XSC
		T+2:25? Stage 1 MECO
		T+2:27? Stage 2 MES, Stage 1 sep
		T+3:52? Fairing sep
		T+4:15? St 2 MECO
		T+4:20? St 2 VECO
	2024	T+4:21? St 2 sep, St 3 MES-1
	2030?	St 3 MECO	190? x 450 ? x 55.1
	2033?	St 3 MES-2
	2034?	St 3 MECO-2
	2035?	St 3 sep
2010 Dec 19		631.36 183 x 35817 x 55.1
2010 Dec 20?		LAM
2010 Dec 22			1436.11 35717 x 35856 x 55.2
2011 Jan 5			1436.13 35719 x 35855 x 55.2 GEO 134.6E

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

May 9,1998

 https://web.archive.org/web/20080504032723/http://digest-archive.degrassi.ca/DD22.htm