Progress M-67

 2009-040A

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11F615A55 No. 367, mission 34P was launched in Jul 2009. It loitered in orbit until STS-127 departed ISS. The automated docking was aborted and taken under manual TORU control by Gennadiy Padalka.

Launch mass 7285 kg. Docking mass 6979 kg. Cargo 2549 kg, including 1125 kg dry.

This was the last 200-series Progress.

PM67
Date	Time	Event	Orbit
2009 Jul 24	1056:56	Launch by Soyuz U Yu15000-112	KB LC1/5
	1101	Blok A burn
	1105:45	Blok I sep
	1436:32	DV1 SKD 66s 27m/s
	1529:36	DV2 SKD 39s 16m/.s
2009 Jul 28	1038:03	SKD burn 2.9s 0.6m/s
2009 Jul 29	1039	SKD burns
	1046	DPO burn
	1048	DPO burn
	1049	At 400m, begin flyaround
	1112:10	Docking with Zvezda aft
2009 Sep 21	0724:56	Undocked from Zvezda
	0728	15s burn, 0.7m/s
		Plazma experiment
2009 Sep 21	1032:03	Plazma TCM 5m/s
2009 Sep 22	1055:28	Plazma TCM 5m/s
2009 Sep 23	0943:19	Plazma TCM 2m/s
2009 Sep 24	1005:59	Plazma TCM 2m/s
2009 Sep 25	1053:39	Plazma TCM 5m/s
2009 Sep 26	0916:22	Plazma TCM 5m/s
2009 Sep 27	0932	Deorbited 166s 87.7m/s
	1020	Impacted in Pacific 47 18 S 139 48W

USA-193

 2006-057A

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The first United Launch Alliance launch. NROL-21 is thought to be an LMSC experimental prototype for the FIA program; originally developed by Boeing, the prime contractor role was transferred during development. After launch, the spacecraft reportedly failed to respond to ground commands. As reentry approached in early 2008, the decision was made to use an AEGIS SM-3 to intercept the satellite.

Mass was about 2300 kg, including 450 kg of hydrazine.

The second stage was placed in a low orbit and probably reentered after a few days.

NRO
Date	Time	Event	Orbit
2006 Dec 14	2100:00	Launch by Delta 7920	V SLC2
		T+1:04 SRM 1-6 off
		T+1:05 SRM 7-9 on
		T+1:26 SRM 1-6 sep
		T+2:11 SRM 7-9 sep
		T+4:23 MECO
		T+4:31 St 1 sep
		T+4:37 SES-1
		T+4:41 Fairing
	2110	T+10:58 SECO-1	185 x 374 x 58.6
	2155	T+55:13 SES-2
	2155	T+55:19 SECO-2	354 x 376 x 58.5
	2157	T+57:50 Stage 2 sep
	2235	T+1:35:50 SES-3
	2235	T+1:35:55 SECO-3
	2320	T+2:20:00 SES-4
	2320	T+2:20:59 SECO-4 depletion	170 x 268 x 52.0 (B, UN)
2006 Dec 14?			91.76 355 x 367 x 58.53 (UN)
2006 Dec 20			91.73 351 x 367 x 58.5
2007 Jun 1			91.30 332 x 343 x 58.5
2008 Feb 1			89.94 270 x 272 x 58.5
2008 Feb 21			89.50 242 x 257 x 58.5
	0330?	Intercept by SM-3 W of Hawaii
	0345?	Debris reentry over Prince George, B.C.
2008 Mar-Apr		debris reentry
2009 Oct 28		Last debris (GH) entry

I Love You,Beth Cooper

 https://welib.org/md5/995c6b2389559ad04e0f8839d9d118da

August 27,2004

 https://en.wikipedia.org/wiki/Coca-Cola

Sirius 6

 2007-057A

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SES Sirius AB's Nordic television satellite at 5E. SES Sirius is the former Nordic Satellite AB (NSAB) and is owned 75 percent SES ASTRA and 25 percent SSC. It is based in Solna.

LM A2100AX with 46 Ku transponders. Launched by Proton M No 53523 and Briz M no 88523. Size is 2.2 x 2.2 x 5.5m, 27m span. Mass is 4600 kg (SES Sirius) or 4385 kg (ILS). The sub-Saharan-Africa beam provided the SES Astra 4A service previously assigned to AMC 12.

Sirius 4
Date	Time	Event	Orbit
2007 Nov 17	2239:47	Launch by Proton-M 53523	KB LC200/39
		T+2:03 St 1 sep
		T+5:33 St 2 sep
		T+5:48 Fairing sep
	2249:33	T+9:46 St 3 sep	-942 x 164 x 51.5
	2251:07	T+11:22 MES-1
	2257?	St 3 reentry
	2258:39	T+18:52 MECO-1	173 x 173 x 51.5
	2348:09	T+1:08:22 MES-2
2007 Nov 18	0004:34	T+1:24:47 MECO-2	258 x 5000 x 50.3
	0209:16	T+3:29:29 MES-3
	0225:48	T+3:46:01 MECO-3	375 x 35812 x 49.1
	0227:09	T+3:47:22 DPB sep	385 x 35681 x 49.1
	0730:03	T+8:50:16 MES-4
	0737:15	T+8:57:28 MECO-4	7002 x 35776 x 17.3
	0752:47	T+9:13:00 Briz 88523 sep	6916 x 35478 x 17.4 (TLE)
2007 Nov 19			821.590 9604 x 35755 x 13.3
2007 Nov 21			887.51 12676 x 35751 x 10.0
2007 Nov 24			1250.94 28391 x 35767 x 1.8
2007 Nov 25	1047	LAM
2007 Nov 26			1431.98 35636 x 35775 x 0.0 GEO 0.03E+1.0E/d

STSS-ATRR

 2009-023A

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Space Tracking and Surveillance System (STSS) Advanced Technology Risk Reduction satellite, formerly the STSS Block 2010 program. The classified MDA satellite will explore "alternate technology" for the STSS. The MDA used NASA to broker launch services with ULA.

The satellite was transferred from MDA to Air Force Space Command in Dec 2010 for use in the space situational awareness network.

Launch by ULA Delta II 7920-10C Azimuth 196 deg.

STSS
Date	Time	Event	Orbit
2009 May 5	2024:26	Launch by Delta 7920	V SLC2W
		T+1:04 SRM 1-6 out
		T+1:05 SRM 7-9 on
		T+1:26 SRM 1-6 sep
		T+2:10 SRM 7-9 out
		T+2:11 SRM 7-9 sep
		T+4:23 MECO
		T+4:31 Stage 1 sep
		T+4:36 SES-1
		T+4:41 fairing sep
	2034:30	T+10:04 SECO-1 over 123.8W 11.5N? at 165.9km	165 x 871 x 98.9?
	2117:18	T+52:52 SES-2 over 44.5E 26.5S?
	2117:39	T+53:13 SECO-2 over 43.5E 24.4S?
	2122:26	T+58:00 Stage 2 sep over 40.3E 8.8S?
		T+58:00 Stage 2 retro
		T+58:42 Stage 2 retro cutoff
	2154:26	T+1:30:00 SES-3 evasive, 5s over 120W 77N
		T+1:30:05 SECO-3
	2207:46	T+1:43:20 SES-4 depletion over Hawaii, 1:34 over 148W 30N
	2209:20	T+1:44:54 SECO-4	180 x 889 x 112.78 over 150W 27N?
			250? x 900? x 112.6
			101.5 792 x 872 x 99.1 (UN)
2009 May 8			866 x 879 x 98.9

Navstar 50

 2009-043A

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GPS IIR-21 (IIRM-8) is SVN 50 (PRN 5) in slot E3, replacing IIA-26. Mass 2059 kg at launch

GPS 49
Date	Time	Event	Orbit
2009 Aug 17	1035:00	Launch by Delta	CC SLC17A
		T+1:03 GEM 1-6 out
		T+1:05 GEM 7-9 on
		T+1:06 GEM 1-6 sep
		T+2:09 GEM 7-9 out
		T+2:11 GEM 7-9 sep
	1039	T+4:23 MECO
		T+4:31 St 1 sep
		T+4:36 St 2 SEIG
		T+4:57 Fairing sep
	1045	T+10:48 SECO-1	174 x 206 x 37.50
		T+1:02:29 SEIG-2
	1138	T+1:03:11 SECO-2	191 x 1241 x 37.95
	1139	T+1:04:04 St 2 sep
	1139	T+1:04:41 TES
	1141	T+1:06:08 TECO
	1141	T+1:06:52 NCS blowdown
	1143	T+1:08:01 St 3 sep	354.77 188 x 20256 x 40.1
	1143	T+1:08:03 St 3 yo deploy
	1221	T+1:46:40 SEIG-3 depletion 32s
	1222	T+1:47:12 SECO-3	204 x 1224 x 32.91
2009 Aug 19	1952	AKM burn	356.86 189 x 20386 x 40.1
	1953	AKM burnout	718.08 20160 x 20209 x 55.12
2009 Sep 4			719.43 20160 x 20275 x 55.11

Salyut - The First Space Station: Triumph and Tragedy

 https://welib.org/md5/1d9765f4fe5b36983a19f3d899b20514