Optus D1

 2006-043B

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D-1 will be an Orbital Star-2 for DTH, internet, voice and transmission. 2299 kg launch, 1005 kg dry, 24 transponders Ku. D-2 to follow.

Mass 2295 kg (EADS PK)

Optus is a subsidiary of SingTel.

Size 4.0 x 3.2 x 2.3m with 17m span.

Date	Time	Event	Orbit
2006 Oct 13	2056	Launch by Ariane 5ECA	CSG ELA3
		T+2:20 PAP sep
		T+3:14 Fairing sep
		T+8:56 EPC MECO
	2105	T+9:02 EPC sep	-1105 x 159 x 6.73
	2105	T+9:06 ESC-A burn
	2140	T+24:44 ESC-A MECO
	2142	T+26:58 DTV 9S sep
	2146	T+30:49 Sylda 5 sep
	2148	T+32:02 Optus D1 sep
	2148	T+32:14 ESC-A sep burn
	2158	T+42:46 Begin LDREX deploy
	2223	T+1:27:05? Complete LDREX deploy
	2224	T+1:28:07 LDREX separates
2006 Oct 15			630.63 252 x 35711 x 7.0
2006 Oct 17			687.43 3073 x 35773 x 4.9
2006 Oct 21	2140?	LAM
2006 Oct 21			1433.30 35686 x 35777 x 0.1
2006 Oct 27			1436.06 35778 x 35793 x 0.1 GEO 164.0E
2006 Nov 7		Relocated
2006 Dec 23			1436.10 35775 x 35798 x 0.0 GEO 160.0E
2010 Apr 30			1436.10 35771 x 35802 x 0.1 GEO 160.0

B-Sat 1A

 1997-016B

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BSAT-1a was launched together with Thaicom 3 on Ariane V95. It will replace the earlier NASDA BS satellites, but is operated by Broadcasting Satellite System Corp. of Tokyo. The coverage beam is over the Japanese islands.

Date	Time	Event	Orbit
1997 Apr 16	2309	Launch by Ariane 44LP	CSG ELA2
	2310	PAP sep T+1:07
	2311	PAL sep T+2:36
	2312	Stage 1 sep T+3:35
	2313	Fairing 01 Sep T+4:45
	2314	Stage 2 sep T+5:43
	2314	Stage 3 burn T+5:48
	2327	Stage 3 shutdown T+18:55
	2328	Thaicom 3 sep T+19:58
	2331	Mini-Spelda top sep T+22:07
	2333	B-SAT sep from H-10-3 T+24:08
1997 Apr 17			630.11 211 x 35725 x 7.0
1997 Apr 21	0315?	Star 30 burn
1997 Apr 21			1414.87 34938 x 35801 x 0.3 GEO 112.2E+5.4E
1997 Apr 30			1436.05 35745 x 35826 x 0.2 GEO 122.1E
1997 May 29			1436.27 35747 x 35833 x 0.1 GEO 121.7E+0.07W
1997 May 31		mv out
1997 Jun 25		mv in	1436.12 35764 x 35809 x 0.1 GEO 111.3E
1997 Jul 28			1436.33 35773 x 35809 x 0.0 GEO 109.9E
1997 Aug 8			1436.10 35783 x 35789 x 0.0 GEO 110.0E
1999 Oct 17			1436.14 35785 x 35789 x 0.0 GEO 110.1E
2006 Aug 3			1436.13 35782 x 35792 x 0.1 GEO 109.6E
2010 Jul 15			1436.15 35779 x 35795 x 0.0 GEO 109.6E

Milstar 4

 2001-009A

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Milstar 2-F2 (DFS-4) was launched in 2001. Mass is 4550 kg? Size is 15.5l 35.4 span

Launch was by Titan 4 K-30/B-41/TC-22. Centaur at sep is 4366 kg and is 8.8l 4.3 dia.

In parking orbit Milstar/Centaur is 23l 4.3d with mass of 24526 kg.

FLT-4 was stationed at 90W in 2002. It was scheduled to be replaced by FLT-6 in 2003 and then to move to 177.5E.

Milstar FLT-4
Date	Time	Event	Orbit
2001 Feb 27	2120:00	Launch by Titan Centaur	CC LC40
		T+2:26 SRMU sep
		T+3:35 Fairing sep
		T+5:25 St 2 MES
	2129	T+9:14 St 2 MECO
		T+9:35 Centaur MES-1
	2131	T+11:34 Centaur MECO-1
			88.49 194 x 205 x 28.6 (ILAM)
		T+1:05:01 Centaur MES-2
		T+1:10:13 MECO-2	634.44 210 x 35949 x 26.7 (ILAM)
	2230:44	T+1:10:44 ILAM epoch
2001 Feb 28	0342	T+6:22:23 MES-3
	0344	T+6:24:36 MECO-3
	0354	T+6:34:49 Centaur sep	1435.09 35764 x 35768 x 4.5 (ILAM)
2008 Dec 23			1436.20 35755 x 35821 x 7.1 GEO 152.0E