Progress M-16M

 2012-042A

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M-16M (No. 416) was launched on a fast rendezvous to demonstrate a quicker path to ISS for future Soyuz crews. Flight 48P.

Mass 7287 kg at insertion, 6936 kg at docking. Cargo 2639 kg including 8 kg Sfera sat.

PM16M
Date	Time	Event	Orbit
2012 Aug 1	1935:13	Launch by Soyuz-U	KB
	1944	Blok-I sep
	2016:43	DV1 49s 20m/s
	2039:13	DV2 29s 11.4m/s
	2142:33	DV3 16s 5.8m/s
	2225:22	DV4 24s 9m/s	276 x 309
2012 Aug 2
	0104	250m range
	0118:43	Docking with Pirs
	0127	Hard dock
	0230?	HO
2012 Aug 3		Remove hatch
2012 Aug 6		Cargo transfers
2012 Aug 7		Cargo transfers
2012 Aug 10		HiMassSEE expt transfer
2012 Oct 31	2308	DPO burn for DAM, 406s, 0.3m/s
2012 Dec 16	1334	Reboost/PDAM 7:50, 0.5m/s 0.9 km
2013 Feb 9	1315:22	Undock
	1318:22	Sep burn 15s
	1619:00	Deorbit 3:28 103.0 m/s
	1622:28	DO CO
	1705	Impact Pacific 44 42S 142 48W

Exploring Mars: The Jet Propulsion Laboratory And The Quest For The Red Planet

 https://welib.org/md5/33745a9438f461d2fb4866a110b6a045

Intelsat 19

 2012-030A

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Will replace Intelsat IS-8 at 166E. C/Ku FSS, DTH and network to Australia, video/mobile services in Asia Pacific to US. One solar array was damaged shortly after fairing separation. It suffered from the same manufacturing defect as the two Estrela do Sul satellites.

IS-19
Date	Time	Event	Orbit
2012 Jun 1	0522:59	Launch by Zenit-3SL
		T+2:30 St 1 sep
		T+3:49 Fairing sep
	0536:21	T+8:31 St 2 sep 184 km	-2174 x 188 x 0
		T+8:41 MES-1
	0536	T+13:47 MECO-1	180 x 1065 x 0
	0606	T+43:48 MES-2
	0613	T+50:18 MECO-2	866 x 35770 x 0
	0623:00	T+1:00:08 DM-SL sep
2012 Jun 2			639.07 797 x 35599 x 0.1
2012 Jun 6			639.07 797 x 35599 x 0.1
2012 Jun 11			1435.20 35667 x 35870 x 0.2 GEO 169.9E+0.2E/d
2012 Jun 27			1436.00 35768 x 35801 x 0.1 GEO 176.0E
2012 Jul 16		Move out of 176E
2012 Aug 8			1437.72 35812 x 35824 x 0.1 GEO 166.2E-0.4W/d
2012 Aug 18		Move in at 166E
2012 Sep 18			1436.11 35784 x 35788 x 0.1 GEO 166.0E
2013 Jun 7			1436.09 35778 x 35794 x 0.0 GEO 166.0E

SJ-10

 2016-023A

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\uni{ 实践十号}{ }

SJ-10 was launched in Apr 2016. Object A was the reentry vehicle and object E is the service module, cataloged after RV separation.

It was suggested by Andrey Krasilnikov that the observed argument of perigee of 315 kg compared to the usual 150 deg represented a launch error, but this has not been confirmed.

SJ10
Date	Time	Event	Orbit
2016 Apr 6	1738	Launch by CZ-2D	JQ
	1748?	Stage 2 sep	89.52 234 x 267 x 42.9
2016 Apr 9			89.50 232 x 266 x 42.9
2016 Apr 10		Orbit raise	89.62 239 x 272 x 42.9
2016 Apr 13			89.59 238 x 270 x 42.9
2016 Apr 14		Orbit raise	89.66 245 x 269 x 42.9
2016 Apr 16			89.64 245 x 268 x 42.9
		Orbit raise	89.73 253 x 268 x 42.9
2016 Apr 18			89.72 253 x 267 x 42.9
	0815	RV separated
	0830	RV landed in Siziwang Banner
2016 Apr 22			89.70 252 x 266 x 42.9
2016 Apr 22		Orbit raise	90.14 254 x 308 x 42.9
2016 May 6			89.96 248 x 295 x 42.9

Payload:

• A1-1 EFILE Evaporation and Fluid Interfacial Effects (IMCAS/Liu)

• A1-2 Phase separation and dynamic clustering in granular gas (IMCAS/Hou)

• A1-3 Thermodynamics of vapor bubble during pool boiling (IMCAS/Zhao)

• A1-4 Thermocapillary convection surface waves (IMCAS/Kang)

• A1-5 Colloidal assembly (IMCAS/ICCSA/Wang)

• A1-6 SCCO Soret coefficients of crude oil (ESA/IMCAS/Verga,Sun)

• A2-1 Wire insulation overload (ignition, soot, smoke), IET-CAS/Kong

• A2-2/3 Coal combustion/pollutant formation (Tsingua/Zhang)

• A2-4 Ignition and burning of solids (IMCAS/Wang)

• A3-1 Solidification and crystal growth (I.Semi.CAS/Zhang)

• B1-1 Space radiation mutagenesis (Dalian Maritime U/Sun), plant materials and tissue equivalent detector devices.

• B1-2 Space radiation, genomic DNA/genetic effects (I Biophys CAS/Hong) mouse cells, fruit flies

• B1-3 Silkworm embryo development (I.Plant.Physio/Eco CAS/Huang)

• B2-1 Signal transduction in plants (IPPE-CAS/Cai)

• B2-2 Biomechanics of cell interactions (IMCAS/Long)

Yahsat 1A

 2011-016A

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Abu Dhabi sat, Al Yah Satellite Communications Co. is a subsid of Mubadala Development Co. of the United Arab Emirates. Astrium/Thales Eurostar 3000 satellite for military and civil comms. Mass 5935 kg (5965 kg with adapter). Size 5.5 x 2.1 x 2.3 m 30.4m span (Arianespace PK), 4.5 x 2.1 x 2.4m 39.4m span (EADS PK)

Station at 52.5E for Mideast, Africa, Europe and SW Asia.

Sylda 5A No. 44A adapter,

"Al Yah" means "the star" (J. Baker, Yahsat, personal comm.)

Yahsat
Date	Time	Event	Orbit
2011 Apr 22	2137	Launch by Ariane 5 VA201 L558	CSG ELA3
		T+2:13 EAP sep
		T+3:04 Fairing sep
		T+8:46 EPC MECO
	2145	T+8:52 EPC sep	-1060 x 169 x 6.1
	2146	T+8:56 ESC-A burn
	2202	T+25:14 ESC-A MECO 9.354km/s 656 km
	2204	T+27:20 Yahsat sep
	2210	T+33:41 Sylda sep
	2211	T+34:56 New Dawn sep
2011 Apr 23			632.94 251 x 35831 x 6.0
2011 Apr 25			848.25 6040 x 35757 x 4.1
2011 May 1			1428.64 35484 x 35797 x 0.1
2011 May 4			1431.62 35671 x 35727 x 0.1 GEO 52.5E+1.1E/d
2011 May 4			1431.64 35669 x 35729 x 0.0 GEO 52.2E+1.1E/d
2011 May 6			1436.00 35775 x 35794 x 0.0 GEO 52.5E
2013 Jun 7			1436.06 35780 x 35791 x 0.0 GEO 52.5E