Navstar 37

 1993-032A

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Navstar 37 (USA 91) was launched on 1993 May 13. It was stationed at plane C-4 and given the ID PRN 07.

Navstar 37
Date	Time	Event	Orbit
1993 May 13	0007:00	Launch by Delta 7925	CC LC17
		T+0:56 SRM 1-3,7-9 out
		T+1:01 SRM 4-6 on
		T+1:02 SRM 1-3 sep
		T+1:03 SRM 7-9 sep
		T+1:57 SRM 4-6 off
		T+2:02 SRM 4-6 sep
		T+4:25 MECO
		T+4:31 VECO
		T+4:33 Stage 1 sep
	0011	Stage 2 TIG (T+4:38)
	0011	Fairing sep (T+4:50)
	0018?	SECO-1 (T+11:37)	186 x 186? x 34.0?
	0027?	T+20 SES-2
	0027?	SECO-2	185 x 732? x 34.0
		T+20:55 spinup
	0028	T+21 Delta sep
	0029	T+22 TES
	0030	T+23 TECO	355.32 171 x 20308 x 37.7
	0031	T+24 Stage 3 sep
	0031	T+24 Yo weight
	0113?	SES-3
		SECO-3 depletion	96.74 472 x 732 x 21.9
1993 May 14	2118?	Star 37XFP burn	716.92 20048 x 20263 x 55.0
1993 Jun 12		In service
1993 Aug 22			717.93 20026 x 20335 x 55.0
1997 Feb 1		Operating at slot C-4
2003 Dec 20		decommissioned

XM-3 (Rhythm)

 2005-008A

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Launch of XM-3 as backup by Zenit-3SL in 2005. Satellite is a BSS702. It will replace XM1 at 85W, XM1 will move to 115W colocated with XM2, which will be replaced by XM4 in 2007. Accourding to some sources, XM-3 is nicknamed Rhythm.

Launch mass 4703 kg, BOL mass 2950 kg. Size 3 x 3.3 x 7m, with 40.4m span.

XM3
Date	Time	Event	Orbit
2005 Mar 1	0351	Launch by Zenit-3SL
		T+2:30 St 1 sep
		T+3:46 PLF sep
	0359	T+8:31 St 2 sep 176 km	-2009 x 178 x 0
	0359	T+8:41 DM MES-1
	0408	T+17:10 MECO-1 207 km	180 x 9452 x 0
	0438	T+47:09 DM MES-2
	0441	T+50:18 MECO-2	675.71 2491 x 35767 x 0.1
	0451	T+1:00:58 DM sep
2005 Mar 1			675.71 2491 x 35767 x 0.1
2005 Mar 4			739.73 5749 x 35682 x 0.1
2005 Mar 5			841.50 5757 x 35760 x 0.5
2005 Mar 7			991.67 17390 x 35735 x 0.3
2005 Mar 9			1411.47 34824 x 35781 x 0.1 GEO 92.6W+6.3/d
2005 Mar 11			1431.13 35595 x 35783 x 0.1 GEO 80.1W+1.2E/d
2005 Mar 11			1435.44 35758 x 35789 x 0.1 GEO 80.1W+0.1E/d
2005 Mar 12			1436.25 35781 x 35797 x 0.1 GEO 80.1W+0.05W/d
2005 Apr 10			1436.18 35784 x 35791 x 0.0 GEO 80.1W+0.03/d

Kosmos 743

  1975-053A

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There is some question as to whether this vehicle used 11A57 or 11A511U: the NK forum in 2010 said it was actually 11A511U. Unlike most Germes flights, Kosmos-743 made several orbital changes.

Kosmos-743
Date	Time	Event	Orbit
1975 Jun 12	1230	Launch by Soyuz-U	Plesetsk
	1234	Blok-I burn
	1238	Blok-I sep
1975 Jun 12			89.63 179 x 332 x 62.8
1975 Jun 13			89.62 180 x 330 x 62.8
1975 Jun 14		Raise apogee	89.77 180 x 345 x 62.8
1975 Jun 15			89.76 180 x 345 x 62.8
1975 Jun 16		Lower orbit	89.14 167 x 296 x 62.8
1975 Jun 19			89.07 167 x 289 x 62.8
1975 Jun 20		Raise apogee	89.24 167 x 306 x 62.8
1975 Jun 24			89.14 166 x 298 x 62.8
		Engine sep
1975 Jun 25
	0348?	Deorbit
	0358?	PO sep
	0402?	Entry
	0418?	Landed

Gambit-3 32

  1971-070A

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KH-8 32 was launched on 1971 Aug 12 by Titan IIIB Agena D from Vandenberg on a 22 day flight. This flight was the first to fly the longer focal length R-5 optical system and marked the transition to the long tank Titan 24B. The vehicle was deorbited over Alaska as part of the VAST 3 experiment to recover a 'payload sensor'.

KH-8 32
Date	Time	Event	Orbit
1971 Aug 12	1530	Launch by Titan 3B Agena D	V SLC4W
	1532	Titan stage 1 sep
	1535	Titan stage 2 sep
	1535	Agena burn
	1540?	Agena MECO
	1630		90.20 137 x 431 x 111.0
1971 Aug 13	0431		90.10 136 x 422 x 111.0
1971 Aug 15	2358		89.68 127 x 389 x 111.0
		Orbit raise
1971 Aug 16	2224		90.04 129 x 423 x 111.0
1971 Aug 19	1623		89.87 130 x 405 x 111.0
		Orbit raise
1971 Aug 20	2220		90.05 131 x 422 x 111.0
1971 Aug 23	1017		89.74 131 x 391 x 111.0
	1946	SRV-1 deorbit opportunity
	1953	Entry
	2020?	SRV-1 recovered
		Orbit raise
1971 Aug 24	0847		90.06 134 x 420 x 111.0
1971 Aug 28	2045		89.83 132 x 399 x 111.0
		Orbit raise
1971 Aug 29	2042		89.98 134 x 412 x 111.0
1971 Sep 1	0238		89.76 133 x 391 x 111.0
1971 Sep 2	2023		89.48 132 x 365 x 111.0
1971 Sep 3		Reentered after 22d
	2223?	SRV-2 ejected
	2230?	Entry
	2255?	SRV-2 recovered
	2347?	VAST 3 controlled reentry in Alaska