GOES-11

 2000-022A

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GOES L mass is 2218 kg. It was another FS-1300 based GOES I series craft launched by ILS Atlas IIA. Span is 26.9m from the solar sail end to the solar panel trim tab. The spacecraft solar sail is a boom with a conical sail on the end; on the opposite site of the bus there is one solar panel array (two panels) with a small tab on the end.

From 2000 to 2006 GOES 11 was kept drifting back and forward between 98W and 115W. In mid-2006 it was moved to the Pacific at 135W.

Date	Time	Event	Orbit
2000 May 3	0707	Launch by Atlas IIA /LPF	CC LC36A
		BECO
		T+4:41 SECO
		T+4:43 Atlas sep
		T+5:00 MES-1
		T+9:36 MECO-1	91.09 180 x 475 x 28.8
		T+22:04 MES-2
		T+23:37 MECO-2	751.09 274 x 41710 x 20.0
	0734	T+27:04 Centaur sep	763.50 275 x 42311 x 20.0
2000 May 3	0822	Solar panel deploy	784.32 459 x 43128 x 20.0
2000 May 4			760.66 240 x 42208 x 20.1
2000 May 5	0330?	T+1d:20:07 AMF-1
2000 May 6			999.32 11233 x 42230 x 5.9
2000 May 7	2200?	T+4d:15:38 AMF-2
2000 May 8			1466.14 29196 x 43548 x 1.3
2000 May 8	0300?	AMF?
2000 May 9			1374.00 26869 x 42255 x 1.1
2000 May 9	2000?	AMF-3	1602.80 35625 x 42353 x 0.3
2000 May 11	1334	AAM
2000 May 11		Renamed GOES 11
2000 May 13			1602.89 35628 x 42354 x 0.3
2000 May 18		T+14d TMF-1
2000 May 19		T+16d TMF-2
2000 May 21		T+17d TMF-3
2000 May 25			1435.57 35756 x 35795 x 0.6 GEO 101.8W+0.12W
2000 May 26			1436.19 35782 x 35794 x 0.2 GEO 104.1W+0.0W
2002 Aug 24			1436.34 35782 x 35799 x 0.3 GEO 105.1W+0.07W
2003 Feb 22			1436.18 35774 x 35802 x 0.1 GEO 113.5W+0.03W
2003 Jul 11		Reverse drift
2003 Dec 21			1435.83 35756 x 35806 x 0.0 GEO 104.1W+0.06E/d
2004 Jun 8		Reverse drift	1436.15 35781 x 35793 x 0.42 96.1W
2004 Jul 18			1436.23 35781 x 35796 x 0.4 GEO 96.5W+0.04W/d
2004 Aug 22		GEO 98W
2005 Mar 16			GEO 111W
2005 Jun 7		Reverse drift	GEO 114.5W
2006 Mar 5			GEO 105W
2006 May 23			1435.93 35767 x 35798 x 0.4 GEO 100.9W
2006 May 24		Move out	1439.91 35796 x 35926 x 0.4
2006 Jun 28		Move in at 135W
2008 Mar 25			1436.03 35779 x 35791 x 0.5 GEO 135.5W