SJ-11-06

 2014-014A

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Shi Jian shiyi hao 06 xing was launched on 2014 Mar 31 into an 0902LTDN SSO.

SJ11-06
Date	Time	Event	Orbit
2014 Mar 31	0258	Launch by CZ-2C	JQ
	0308?	Stage 2 sep	98.60 680 x 702 x 98.3
2014 Jul 19			98.68 687 x 703 x 98.3

Gonets 2013

 2013-048A

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Planned launch of 'Blok no. 12' (Gonets-D1M Block 372AS71 No. 12) with satellites 372AS11 No. 14, 16, 17 using Rokot 14A05 No. 4926391838 and Briz-M 72519.

Gonets-M
Date	Time	Event	Orbit
2013 Sep 11	2323:04	Launch by Rokot	PL LC133/3
	2325:06	Stage 1 MECO
	2325:54	Fairing sep
	2328?	Stage 2 MECO
	2328:09	Stage 2 sep
	2328:15	MES-1
	2337:44	MECO-1	100? x 1500 x 82.6
2013 Sep 12	0037:24	MES-2
	0038:17	MECO-2
	0107:13	Spacecraft sep
2013 Sep 13			116.04 1495 x 1510 x 82.5

Himawari 8

 2014-060A

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The geostationary meteorological satellite Himawari 8 was built by MELCO for JMA, as a successor to the MTSAT series. Size 8 m high. Box + dish + 1 pan Mass 3500 kg launch 1300 kg dry. Launch by MHI on H-IIA 202 F25 with 4S fairing on 96 deg azimuth.

GMS8
Date	Time	Event	Orbit
2014 Oct 7	0516:00	Launch by H-IIA F25	TNSC
		T+1:36 SRM out
		T+1:48 SRB sep
		T+4:05 Fairing sep
	0522	T+6:36 Stage 1 MECO
	0522	T+6:44 Stage 1 sep 222 km, 5.3 km/s
		T+6:50 SES-1
	0528	T+12:12 SECO-1 271 km, 7.7 km/s	250? x 300? x 30?
	0539	T+23:50 SES-2 264 km, 7.7 km/s
	0543	T+27:07 SECO-2
	0543	T+27:57 separation
2014 Oct 8			795.22 8227 x 35882 x 8.8
2014 Oct 9			1335.44 31745 x 35839 x 0.4
2014 Oct 15			1436.01 35756 x 35813 x 0.1 GEO 140.8E
2014 Nov 25			1436.14 35784 x 35791 x 0.0 GEO 140.8E

Payload:

• AHI Advanced Himawari Imager: 3 vis at 0.5-1km, 3 NIR 1-2 km res., 10 IR bands; 10 minute cadence

WGS-6

 2013-041A

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Third Block II WGS satellite supporting 2.4-3.6 Gbps data transfer in X and Ka band. Funded by Australia. Control from 3SOPS/Schreiver.

Mass 6100 kg.

WGS 6
Date	Time	Event	Orbit
2013 Aug 8	0029	Launch by Delta 4M+(5,4)	CC SLC37B
		T+1:31 SRM 1-2 burnout
		T+1:33 SRM 3-4 burnout
		T+1:40 SRM 1-2 sep
		T+1:42 SRM 3-4 sep
		T+3:27 Fairing sep
		T+4:07 MECO
		T+4:14 St 1 sep
		T+4:27 DCSS SES-1
	0049	T+20:32 DCSS SECO-1	185 x 6880 x 25.6
		T+28:22 DCSS SES-2
	0100	T+31:31 SECO-2	439 x 66900 x 24.0
	0109	T+40:38 DCSS sep from WGS
	0120?	CCAM
	0156?	End DCSS depletion

Eutelsat 3B

 2014-030A

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Astrium Eurostar 3000 satellite, 51 transponders for Africa, Mideast, Central Asia and S America. 5967 kg. Size 7.5m high 31m span, 12 kW power.

Eut3B
Date	Time	Event	Orbit
2014 May 26	2109:59	Launch by Zenit-3SL	SL Odyssey
		T-0:03.5 Go Inertial
		T+2:27 St 1 sep
		T+3:48 Fairing sep 118 km
		T+7:12? St 2 shutdown
		T+8:28 St 2 sep	-2239 x 185 x0
	2118:36	T+8:38 DM-SL MES-1
	2123:12	T+13:17 DM-SL MECO-1 180 x 407 x 0
	2153:45	T+43:47 DM-SL MES-2
	2200:38	T+50:44 DM-SL MECO-2 532 km	381 x 35799 x 0
	2210:28	T+1:00:34 SC Sep
		T+6:02:55 Apo-1	385 x 35646 x 0
2014 May 27			630.70 368 x 35599 x 0.0
2014 May 28			734.98 5580 x 35619 x 0.0
2014 May 29			957.35 15980 x 35616 x 0.1
2014 Jun 2			1153.65 24494 x 35623 x 0.0
2014 Jun 5			1428.57 35625 x 35653 x 0.0
2014 Jul 19			1436.08 35779 x 35793 x 0.1 GEO 3.1E

Intelsat 601

 

1991-075A

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The satellite was a spin stabilized 5.4 m high, 3.6m diameter cylinder with an extendable solar array skirt (deployed height was 11.8m). The 1908 kg dry mass of the satellite was increased to 4260 kg when fuelled (BOL mass was 2560 kg). The masses of the various components of the Ariane 44L launch vehicle are tabulated below:

 

Ariane mass budget
Element	Dry mass	Fuel	Total
PAL (4)			17991
L220	18254	387244	405498
St 2	3696	35479	39175
H10	1279	10586	11865
Case a equipement	723		723
Adapter	70		70
Intelsat 601	1908	2352	4260
Fairing	815		815
Ariane total			480397

Intelsat VI~F-1
Date	Time	Event	Orbit
1991 Oct 29	2308:08	Launch by Ariane 44L (V47)	CSG ELA2
	2309	PAL1 and 2 sep (T+2:29)
	2309	PAL3 and 4 sep (T+2:30)
	2310	Stage 1 sep (T+3:33)
	2310	Stage 2 MES (T+3:36)
	2311	Fairing sep (T+4:19)
	2312	Stage 2 sep (T+5:45)
	2312	Stage 3 MES (T+5:50)
	2326:00	Stage 3 MECO (T+17:52)
	2330:45	Stage 3 sep (T+22:37)
	2331:39	Stage 3 sep burn (T+23:31)
1991 Oct 30	0430?	R4D test burn	634.83 280 x 35899 x 7.1
1991 Oct 31	0137s	LAM-1 R4D main burn 1
1991 Oct 31	1200		715.97 4532 x 35733 x 4.44
1991 Nov 1	0200?	LAM-2	1087.51 21572 x 35732 x 0.89
1991 Nov 2	1400?	LAM-3
1991 Nov 3			1436.01 35772 x 35797 x 0.0 GEO 38.0W
1991 Oct		Tests	GEO 38W
1991 Nov 14			1436.12 35673x35900x0.05 GEO 37.00W-0.01/d
1991 Nov		Spot beam malfunction discovered
1992 Jan 27			1436.15 35682 x 35892 x 0.1 GEO 37.2W+0.02W
1992 Feb 16		drifting
1992 Mar		Spot beam repaired
1992 Mar 27		In service
1992 Apr 4		mv in	1436.05 35773 x 35798 x 0.1 GEO 27.6W
1994 Feb 26			1436.12 35783 x 35790 x 0.0 GEO 27.5W
1996 Dec 27			1436.13 35777 x 35796 x 0.0 GEO 27.5W
1997 Oct 8		mv out	GEO 28W
1997 Oct 20		mv in	GEO 34W
1997 Oct 25			1436.04 35777 x 35793 x 0.0 GEO 34.5W
1999 Jun 15			1436.10 35784 x 35789 x 0.0 GEO 34.5W
2002 Jun 28		Move to 32E and then 64E
2002 Jul 11		mv in	1436.13 35783 x 35790 x 0.0 GEO 32.9E
2002 Sep 29		mv out	1436.06 35781 x 35789 x 0.0 GEO 33.0E
2002 Nov 1		mv in	1435.80 35754 x 35806 x 0.0 GEO 64.3E
2003 Sep 2			1436.09 35778 x 35794 x 0.0 GEO 64.3E
2006 Aug 3			1436.01 35780 x 35793 x 1.8 GEO 64.3E
2007 Oct 2		mv out from 63E
2007 Nov 4		Move in 47E
2011 Oct 14			1436.06 35784 x 35787 x 6.5 GEO 47.4E

The rich : from slaves to super-yachts : a 2,000-year history

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