LaoSat 1

 2015-067A

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LaoSat 1 will launch on a CZ-3B. It is a DFH-3 satellite owned by Lao Satellite Joint Venture Company (involving Lao government, China APMT), positioned at 128.5E.

Laosat 1
Date	Time	Event	Orbit
2015 Nov 20	1607	Launch by CZ-3B	XSC
		T+2:21 Booster sep
		T+2:35 St 1 sep
		T+2:39 St 1 burn?
		T+3:55 Fairing
		T+6:37 St 2 sep
	1613	T+6:44 St 3 MES-1
	1617	T+10:19 St 3 MECO-1	208 x 635 x 27.1
	1628	T+21:03 St 3 MES-2
		T+24:01 St 3 MECO-2	201 x 35824 x 27.1
	1631	T+24:20 St 3 RCS cutoff
	1632	T+25:40 Payload sep
2015 Nov 27			752.45 159 x 41892 x 18.3
2015 Nov 30			1436.14 35781 x 35793 x 0.1 GEO 128.5E

Progress M-26M

 2015-008A

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Spacecraft 425, mission 58P. Mass 7289 kg including 880 kg prop, refuelling prop 436 kg, 50 kg O2, Rodnik water, 420 kg; cargo in GO 1465 kg, total cargo 2372 kg.

PM26M
Date	Time	Event	Orbit
2015 Feb 17	1100:17	Launch by Soyuz-U	KB
		T+4:45 Blok A MECO
		T+4:47 Blok A sep
		T+8:44 Blok I MECO
	1109:06	T+8:49 Blok I sep	88.73 186 x 237 x 51.7
	1153:21	DV1 37.4s 14.57m/s
	1216:30	DV2 12.9s 4.7m/s	233 x 255
	1314:23	DV3 20.1s 7.6m/s
	1403:46	DV4 24.9s 9.60m/s	262 x 287
	1645	Aligned with docking port
	1657:13	Docked with Zvezda
2015 Feb 26	0916	Reboost 4:45 0.62m/s
2015 Mar 3	0800	Reboost 3:17 0.43m/s
2015 Mar 18	2345:00	Reboost 4:18 0.6m/s
2015 Apr 2	1832	Reboost 3:03 0.4m/s 59kg
2015 Apr 23	0522	COLA DAM 2:28 0.3m/s 45kg?
2015 May 6	0515:00	Reboost 12:17 1.34m/s 194 kg 693s
2015 May 16	0114	Reboost aborted, DPO-1 problem
2015 May 18	0030	Reboost 32:03 burn 1.89m/s 305 kg
2015 May 28		DPO-1 test 10s
2015 Jun 8	1958	COLA PDAM 5:22
2015 Jun 18	1059	Reboost 0.5m/s 4:08
2015 Jul 10	0254:00	Reboost 1.22m/s 10:57 180kg
2015 Jul 26	0348	COLA PDAM (Iridium) 252s 0.5m/s
2015 Aug 12		HC
2015 Aug 14	1019:19	Undocking from Zvezda
	1023	Sep-1
	1328:00	Deorbit 101.8m/s
	1417	Impact in Pacific 47 05 24 S 137 55 48W

Gsat 6

 2015-041A

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ISRO Insat 4E (GSAT-6), I2K bus. Mass 2100 kg. 440N LAE

The CUS has a thrust of 73.6 kN for 720s and carries 12800 kg of prop. Second stage thrust for this mission is improved to 799 kN from 720; core stage burn is 6 s longer at 4815 kN thrust and the GSOMs burn for 149s at 759 kN, higher thrust than reported for previous missions.

GSAT6
Date	Time	Event	Orbit
2015 Aug 27	1122	Launch by GSLV-D6	SDSC SLP
		T+2:29 SOM cutoff 71 km 2.3917 km/s
		T+2:30 St 2 ignition
		T+2:31 St 1 sep 72 km 2.3918 km/s
		T+3:50 Fairing sep 115 km 3.448 km/s
		T+4:49 St 2 cutoff 131.8 km 4.908 km/s
		T+4:43 St 2 sep
	1126	T+4:54 CUS ignition
	1138	T+16:42 CUS shutdown 205.1 km 9.7856 km/s
	1139	T+17:04 CUS sep 214 km 9.779 km/s
2015 Aug 28	0305	LAM-1 3385s	8408 x 35708 x 7.5
2015 Aug 29	0540:53	LAM-2 2663s	26998 x 35682 x 0.12
2015 Aug 30	0216	LAM-3 580.3s	35634 x 35681 x 1.2
2015 Aug 30		S-band antenna deployed
2015 Sep 1			1431.29 35671 x 35713 x 1.2
2015 Sep 1			GEO 78.0+?E/d
2015 Sep 10			1436.04 35757 x 35813 x 1.2
2015 Sep 28			1436.09 35750 x 35821 x 1.1 GEO 83.1E