USA-186

 2005-042A

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USA 186 was launched by the final Titan rocket to a 0945 LTDN SSO, the west plane.

USA 186
Date	Time	Event	Orbit
2005 Oct 19	1805:00?	Launch by Titan 4 B-26	V SLC4E
		T+2:13 St 1 burn
		T+2:28 SRMU sep
		T+3:30 PLF sep
		T+5:26 St 1 sep
		T+9:18 St 2 MECO
	1814	T+9:30 St 2 sep
			96.7 164 x 1046 x 97.8 (UN)
			95.31 165 x 901 x 97.9 (42B)
		In 0945LT SSO
2005 Oct 28			264 x 1050 x 97.9
2006 Mar 24			264 x 1030 x 97.9
2006 Dec 22			97.47 264 x 1010 x 97.9
2007 Jan 11		small reboost
2007 Jan 30			97.51 262 x 1016 x 97.9
2008 Mar 14			97.16 263 x 982x 97.9
2008 Mar 20		Large reboost	97.63 262 x 1028 x 98.0
2008 May 19			97.54 261 x 1020 x 97.9
2008 Dec 10		Reboost
2009 Apr 9		Reboost
2011 Apr 18			97.26 256 x 997 x 97.9
2013 Aug 29			97.54 263 x 1018 x 97.9
2013 Sep 26		In 0943LT plane	97.46 260 x 1012 x 97.9
2013 Dec 10?		Orbit change out of SSO
2013 Dec 17		Recovered in 0930LT plane at 2.7 hr/yr	97.20 260 x 988 x 96.9
2014 May 30			96.5 260 x 929 x 96.9
2014 Jul 1?		Orbit change to SSO
2014 Sep 9		Recovered in 0806LT plane at 0.13hr/yr	91.61 266 x 440 x 96.9
2014 Sep 13			91.58 263 x 440 x 96.9
2014 Sep 19			91.92 287 x 449 x 96.9
2014 Dec 22			91.32 260 x 417 x 96.9
2014 Dec 28		Orbit raise	91.76 271 x 450 x 96.9
2015 Feb 17			91.44 261 x 429 x 96.8
2015 Apr 3		Orbit raise	91.99 267 x 477 x 96.9
2016 Mar 9			91.36 261 x 421 x 96.9
2016 Mar 14		Orbit raise	91.76 260 x 460 x 96.9
2016 May 30			91.44 262 x 436 x 96.9

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)