Eutelsat W5

 2002-051A

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Eutelsat W5 was the payload for the first Delta IV. Spacebus 3000B2 built by Alcatel/Cannes. Launch mass 3170 kg. The upper stage has an RL10B-2 engine and a 4-m fairing.

Debris appears to have come off the second stage during its second burn, cataloged at intermediate inclinations.

Eutelsat W5
Date	Time	Event	Orbit
2002 Nov 20	2239:00	Launch by Delta IV M+(4,2)	CC SLC37B
		T+1:34 GEM60 x2 burnout
		T+1:40 GEM60 x2 sep
		T+4:04 MECO
		T+4:15 CBC sep
	2243:29	T+4:29 SES-1 141 km
		T+4:39 Fairing 151 km
		T+12:54 Perigee positive
	2252:06	T+13:06 SECO-1	185 x 595 x 27.3 (PK)
	2302:26	T+23:26 SES-2 4:59
	2307:25	T+28:25 SECO-2	538 x 35966 x 13.5 (PK)
		T+37:11 Spinup
	2316:35	T+37:35 Stage 2 sep	562 x 35777 x 13.6
		Depletion	556 x 34635 x 13.1
2002 Nov 20			637.94 562 x 35777 x 13.6
2002 Nov 20		Delta RB	615.71 556 x 34635 x 13.1
2002 Nov 21		LAM-1
2002 Nov 24			1016.17 18424 x 35782 x 2.8
2002 Nov 25			1016.14 18424 x 35781 x 2.8
2002 Dec 1	0500?	LAM-2
2002 Dec 4			1436.12 35780 x 35793 x 0.1 GEO 53.5E
2002 Dec 14		Move to 70E
2003 Jan 3			1436.18 35682 x 35893 x 0.1 GEO 70.4E
2006 Aug 8			1436.09 35770 x 35802 x 0.0 GEO 70.5E
2008 Jun 17		4 transp. shut down after power problem
2012 Mar 1		Renamed EUTELSAT 70A
2013 Jan 16			1436.12 35767 x 35806 x 0.1 GEO 70.4E
2013 Jan 16		Move out, drift W
2013 Feb 20		Move in, renamed Eutelsat 25C	1436.13 35767 x 35806 x 0.0 GEO 25.5E
2013 Apr 13			1436.19 35781 x 35795 x 0.0 GEO 25.5E
2013 Oct 30			1435.22 35748 x 35790 x 0.1 GEO 25.6E
2013 Oct 31		Move out
2013 Nov 14		Move in	1436.07 35781 x 35791 x 0.0 GEO 33.1E
		Renamed Eutelsat 33B
2015 Mar 16			1436.11 35782 x 35791 x 0.0 GEO 33.1E
2015 Oct 14			1436.02 35779 x 35790 x 0.1 GEO 33.2E