Thor 5

 2008-006A

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Telenor Satellite Broadcasting's Thor 5 (Thor 2R) built by Orbital. Mass 2012 kg or 1960 kg (2024 kg with adapter?), 1090 kg dry. 

Thor 2R
Date	Time	Event	Orbit
2008 Feb 11	1134:00	Launch by Proton	KB LC200/39
		T+2:03 St 1 sep
		T+5:33 St 2 sep
		T+5:45 GO sep
	T+9:33 St 3 MECO
	1143:45	T+9:45 St 3 sep	-682 x 178 x 51.58
	1145:19	T+11:19 Briz MES-1
	1150:56	T+16:56 MECO-1	173 x 173 x 51.6
	1201?	St 3 reentry
	1242:30	T+1:08:30 MES-2
	1258:56	T+1:24:56 MECO-2	298 x 5000 x 50.3
	1457:56	T+3:23:56 MES-3
	1516:58	T+3:42:58 MECO-3
	1518:12	T+3:44:12 DTB sep	496 x 36846 x 49.1
	2034:02	T+9:00:02 MES-4
	2044:32	T+9:10:32 MECO-4
	2056:50	T+9:22:50 Briz sep in GEO	36746 x 36840 x 0.0
	2300:00	T+11:26:00 SOZ-6 burn 25s
	2300:25	T+11:26:25 SOZ-6 CO
2008 Feb 12	0226		1473.52 35946 x 37085 x 0.12 GEO 51.2E+9W/d
2008 Feb 19		mv	1451.48 35953 x 36221 x 0.1
2008 Feb 23		mv in	1439.31 35774 x 35924 x 0.1 GEO 16.5W
2008 Feb 29		mv out
2008 Mar 4			1426.29 35585 x 35603 x 0.1 GEO 7.4W+2.4E/d
2008 Apr 28		mv in at 0.7W	1436.06 35767 x 35804 x 0.07 GEO 0.7W
2010 May 2			1436.08 35775 x 35796 x 0.0 GEO 0.7W

People: August 23,2010

 https://welib.org/md5/14263b148099e257f789ceac7070ec1a

Amos 2

 2003-059A

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IAI MBT Div. to build Amos-2. Spacecom Ltd./Tel Aviv is service provider for Amos-2; the satellite was delivered on orbit by IAI. Mass 1350 kg full (or 1374 kg), 646 kg dry, size 2.7 x 2.1 x 2.4m span 11.0m. It will backup Amos 1 at 4W and include service to the eastern US. Launch by Starsem Soyuz-Fregat in Dec 2003.

Followon AMOS HP with 20 Ku-band transponders and 2600 kg mass?

Amos 2
Date	Time	Event	Orbit
2003 Dec 27	2130:00s	Launch by Soyuz-FG/Fregat ST12	KB PL31/6
		T+1:58 BVGD sep
		T+4:13 Fairing sep
		T+4:48 Blok A sep
		T+4:58 KhO sep
		T+8:45 Blok I MECO
	2138:48	T+8:48 Blok I sep	58 x 190 x 51.8
	2138:53	T+8:53 SOZ-1 burn
	2139:49	T+9:48.5 MES-1 20.5s
	2140:09	T+10:09 MECO-1 EPO	190? x 190?
	2215?	Blok I reentry
		T+1:09:29 SOZ-2
	2240:24	T+1:10:24 MES-2 ascending node=10.25W 25S 25W, 659s
	2251:23	T+1:21:23 MECO-2 intermediate 16N 2E	250? x 35780 x 49?
2003 Dec 28	0403:34	T+6:33:34 SOZ-3 burn
	0404:29	T+6:34:29 MES-3 over 90E 0N, 137s
	0406:46	T+6:36:46 MECO-3	4407 x 35788 x 23.63
	0406:47	T+6:46:47 Fregat sep	4409 x 35779 x 23.58
	0446:47	T+7:16:47 SOZ-4 Fregat depletion
	0447:02	T+7:17:02 SOZ cutoff
2003 Dec 29			714.42 4409 x 35779 x 23.58
2003 Dec 30	0317	ABM-1 46min burn	19000 x 35800
	2040?	Apogee
2003 Dec 31	1350	ABM-2 17min burn	34000 x 35800
2004 Jan 5			1402.99 34439 x 35832 x 0.3
2004 Jan 12		On Station	GEO 4W
2004 Feb 19		Delivered to Spacecom
2006 Aug 1			1436.07 35777 x 35794 x 0.1 GEO 4.0W

Seventeen: April 2010

 https://welib.org/md5/ce0d1381c9c6c6da1dbad191ea0172a1