Intelsat 10

 2004-022A

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IS10 is a 5575 kg Eurostar 3000. The satellite uses a plasma thruster for stationkeeping. Dry mass is 3125 kg.

Intelsat 10
Date	Time	Event	Orbit
2004 Jun 16	2227:00	Launch by Proton-M 53506 / Briz-M 88509	KB LC200/39
		T+2:03 St 1 sep at 41.8 km	-6160? x 45? x 50.5
		T+5:29 St 2 sep at 120 km	-4920? x 130 x 51.4
		T+5:42 Fairing sep	-4900? x 135? x 51.4
		T+8:36 141 km alt
		T+9:38 Stage 3 sep
	2237	T+10:00 147 km alt	-900? x 149 x 51.6
	2238	T+11:12 Briz MES-1
	2245	T+18:52 Briz MECO-1	173 x 173 x 51.5
	2335	T+1:08:12 Briz MES-2
	2352	T+1:24:54 MECO-2	258 x 5000 x 50.3
2004 Jun 17
	0155	T+3:28:45 MES-3
	0205	T+3:38:15 MECO-3
	0205	T+3:38:30 DTB jettison over 45W 0N	246.32 309 x 12967 x 49.7
	0207	T+3:40:20 MES-4
	0214	T+3:47:03 MECO-4	414 x 35849 x 49.0 (TLE)
	0720s	T+8:53:09 MES-5
	0725s	T+8:58:49 MECO-5	4184 x 35804 x 23.7 (TLE)
	0737	T+9:10:20 Briz sep
	0942s	T+11:15:00 Briz depletion
2004 Jun 20?		LAM-1
2004 Jun 21		LAM-2	1251.90 28436 x 35761 x 1.9
2004 Jun 23	1100?	LAM-3	1432.88 35678 x 35678 x 0.1
2004 Jul 6			1436.59 35787 x 35805 x 0.2 GEO0.02E+0.6E
2004 Jul 8			1436.26 35777 x 35802 x 0.1 GEO 0.7E+0.05W
2004 Jul 20			1436.02 35768 x 35801 x 0.1 GEO 0.9E
2004 Aug 19		Relocate to 1.0W
2004 Sep 2			1436.10 35782 x 35790 x 0.0 GEO 1.0W
2006 Aug 8			1436.06 35781 x 35790 x 0.0 GEO 1.0W