Kosmos 2413

2004-053A

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Two Uragan, No 796/797 and one Uragan-M No 712 (No 12L ) were launched in Dec 2004 and given the names Kosmos-2411 to Kosmos-2413. They were placed in slots 1,7,8 of orbit plane 1.

The Uragan satellites were built by Polyot, with the Uragan-M developed by Reshetnev NPO-PM. Masses were 1370 kg each.

Originally the GLONASS web site said Kosmos-2411 was sat 712, but later this was corrected to 796 (formerly assocated with 2413).

712 was retired to backup status on 2011 Dec 14 but reactivated 2012 Oct; it was finally deactivated on 2012 Dec 21.

796 was removed from the constellation on 2008 Oct 18.

Kosmos-2411
Date	Time	Event	Orbit
2004 Dec 26	1353:31	Launch by Proton-K 410-09 DM 11S861 104L	KB LC81/23
		T+2:06 St 1 sep
		T+3:17 GO sep
	1359:09	T+5:38 St 2 sep
	1403:11	T+9:40 St 3 MECO
	1403:23	T+9:52 St 3 sep	157 x 386 x 65.0
	1442:50	T+49:19 DM MES1
	1448:37	T+55:06 DM MECO 1
	1735:39	T+3:42:08 DM MES2
	1738:02	T+3:44:31 DM MECO 2
	1738:17	T+3:44:46 DM sep	19134 x 19143 x 64.9

DFH-54

 2002-024B

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950 kg satellite launched by CZ-4B from TYSC. Advertised as supporting the 2008 Olympic Games. FY-1D still operating in Dec 2008.

FY-1D
Date	Time	Event	Orbit
2002 May 15	0150	Launch by CZ-4B	TY
	0152	T+2:32? St 1 sep
	0152	St 2 burn
	0152	T+2:47? Fairing sep
	0156	T+6:48? Stage 2 MECO
	0156	T+6:49? St 2 sep
		Stage 3 burn
	0200?	Stage 3 MECO
	0202	T+12:29? FY-1D sep
	0203?	Adapter sep?
	0203	T+13:34? HY-1 sep
2002 May 17			102.19 851 x 873 x 98.8
2004 Feb 12			102.19 850 x 873 x 98.7

JCSAT 6

 1999-006A

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JCSAT 4A (also called JCSAT 6) is an HS-601, delivered May 1998, 32 Ku tsp. to be launched by Atlas 2AS in 1999 into supersynch transfer orbit. Launch mass is 2900 kg, dry mass is 1226 kg.

The satellite will replace JCSAT-4 which will become a spare; that replaced JCSAT-1 in 1997. Launch of JCSAT-6 by Atlas 2AS was delayed following the SCP problems with several on-orbit HS-601s. JCSAT 6 will operate at 124E.

JCSAT 6
Date	Time	Event	Orbit
1999 Feb 16	0145:26	Launch by AC-152	CC LC36A
		T+0:55 SRM 1-2 burnout
		T+0:58 SRM 3-4 burn
		T+1:06 SRM 1-2 sep
		T+1:54 SRM 3-4 burnout
		T+1:56 SRM 3-4 sep
		T+2:43 BECO
		T+2:47 Booster sep
		T+3:23 Fairing sep
		T+5:01 MECO
		T+5:03 Atlas sep
		T+5:05 MES1
	0155:08	T+9:42 MECO1	89.80 153 x 375 x 27.6
	0209:54	T+24:29 MES2
	0211:46	T+26:20 MECO2	2109.90 166 x 96061 x 20.9
	0215:33	T+30:07 Centaur sep	(ILAM) 2101.90 166 x 95786 x 20.9
	0215	perigee from TLE
		T+1:10:47 Centaur depletion	(ILAM) 2062.10 169 x 94406 x 20.9
1999 Feb 16			2132.20 258 x 96736 x 24.1
1999 Feb 16	2001	Apogee 1 at 91W
1999 Feb 18	0733	Apogee 2 at 94E, LAM-1
1999 Feb 18			2486.36 11949 x 96885 x 7.7
1999 Feb 20	0100	Apogee 3 at 168W
1999 Feb 21	1300?	LAM-2
1999 Feb 21	1540	Apogee 4 at 28W
1999 Feb 23	2233	Apogee 5 at 134W
1999 Feb 25			3293.80 36209 x 97697 x 1.2
1999 Feb 26	0526	Apogee 6 at 120E
1999 Feb 28	1223	Apogee 7 at 14E
1999 Mar 1	1551	Perigee at 141E
1999 Mar 1?		LAM at perigee
1999 Mar 6			1436.32 35765 x 35816 x 0.1 GEO 120.6E+0.06W
1999 May 8		mv out	GEO 120E
1999 May 24		mv in	GEO 123E
1999 May 29			1436.09 35782 x 35790 x 0.1 GEO 123.9E
1999 Nov 7			1436.14 35773 x 35801 x 0.1 GEO 124.1E
2006 Aug 2			1436.13 35782 x 35791 x 0.0 GEO 124.0E

Ekspress AM-33

 2008-003A

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KSvyaz satellite, NPO-PM 767 (Ekspress-2000) bus. Launch 2008 to 96.5E. Payload by Thales Alenia. 

EX AM-33
Date	Time	Event	Orbit
2008 Jan 28	0018:00	Launch by Proton	KB LC200/39
		T+2:03 Stage 1 sep
		T+2:55 GO sep
		T+5:30 Stage 2 sep
	0027	T+9:32 Stage 3 MECO
	0027	T+9:44 Stage 3 sep
	0029	Briz MES-1
	0035:01	T+17:01 Briz MECO-1 285m/s	173 x 173 x 51.6
	0042?	Stage 3 reentry
	0125:18	T+1:07:18 Briz MES-2
	0143:26	T+1:25:26 Briz MECO-2?	276 x 4999 x 48.8
	0347:30	Briz MES-3
	0404:56	Briz MECO-3
	0406:18	DTB sep	405 x 35550 x 46.2
	0905:50	Briz MES-4
	0917:48	Briz MECO-4
	0918:56	Briz sep	33985 x 35559 x 0.05
	1120:10	Briz depletion burn 39m/s
2008 Feb 1			1422.58 35257 x 35785 x 0.1 GEO 70.3E+3.4E/d

THEOS

 2008-049A

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Thaichote, the Thai Earth Observation Sat (THEOS), for Thai GISTDA, Min of Science and Tech. EADS Astrium AstroSat bus hexagon + panel, 2.1 m dia 2.4m high 750 kg, 22 km swath, 2m res pan and multispectral imager, 90 km FOV, 15m res; AstroSat-500 like Rocsat 2. System designed to be similar to SPOT.

Launch by Dnepr.

Owned by Thai Ministry of Science and Technology's Geo-Informatics and Space Technology Development Agency (GISTDA) Control center at Sri Racha, Chonburi province.

THEOS
Date	Time	Event	Orbit
2008 Oct 1	0637:16	Launch by Dnepr	Yasniy
		T+1:49? Stage 1 sep
		T+4:36? GO
		T+4:41? St 2 sep
	0642	T+4:45? DU on
	0652?	Plume shield sep
	0652?	DS MECO
	0652?	Satellite separation
2008 Oct 2			98.42 672 x 692 x 98.8
2008 Oct 3		Begin orbit raise
2008 Oct 9			100.75 792 x 796 x 98.8
2008 Oct 12			101.33 820 x 822 x 98.8
2008 Oct 15		Final orbit	101.41 824 x 826 x 98.8
2008 Oct 20			101.41 824 x 826 x 98.8

Payload:

• Pan imager, 2m res GSD, 22 km swath with SiC Cass. telescope

• Multispectral imager, 15m GSD, 90 km swath, dioptic camera

The New York Times Almanac 2007

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Intelsat 903

 2002-016A

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This was a Loral 1300 satellite,mass 1972 kg dry. Launch from PL81/23 by Proton-K/DM3. Station at 34.5W.

Intelsat 903
Date	Time	Event	Orbit
2002 Mar 30	1725:00	Launch by Proton-K/DM3
	1727	T+2:03 St 1 sep
	1727	St 2 burn 3.5min
	1730	T+5:31 St 2 sep
	1730	T+5:31 St 3 MES
	1730	Fairing sep
	1734:44	T+9:44 St 3 MECO
	1734:44	T+9:44 St 3 sep, suborbital	-630 x 161
	1735:38	T+10:38 DM casing sep	-630 x 161
	1740:46	T+15:46 DM3 No 28L burn 1 66s
	1741:52	DM MECO-1, EOI	168 x 168 x 51.6
	1750?	St 3 reentry
	1838:09	T+1:13:09 DM MES-2 7:18
	1845:27	DM MECO-2	630.9 166 x 35814 x 51.67
	2339:00	T+6:14 DM MES-3 90s
	2340:30	DM MECO-3
2002 Mar 31	0007:51	T+6h42:51 DM sep	697.00 3475 x 35848 x 25.0
	0150:51	T+8:25:51 DM CCAM
	0238	DM end of ops
2002 Mar 31			697.00 3475 x 35848 x 25.0
2002 Apr 3		LAM-1	850.76 10885 x 35841 x 11.0
2002 Apr 5		LAM-2	1332.60 31653 x 35817 x 0.7
2002 Apr 6	0540?	LAM-3	1436.04 35773 x 35797 x 0.1 GEO 26W
2002 May 10		mv out	1436.09 35768 x 35804 x 0.0 GEO 25.8W
2002 May 25		mv in	1436.10 35780 x 35792 x 0.0 GEO 34.5W
2002 Jul 18			1436.11 35776 x 35796 x 0.0 GEO 34.5W
2006 Aug 8			1436.11 35768 x 35807 x 0.0 GEO 34.5W

Astra 2C

 2001-025A

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HS-601HP, 2001 launch on Proton. At 28.2E for service to British Isles. Launch mass 3643 kg. 26m span, 10.1m high deployed.

Astra 2C
Date	Time	Event	Orbit
2001 Jun 16	0149:00?	Launch by Proton	KB LC81/23
		T+2:00 St 2 MES
		T+2:06 St 1 sep
		T+5:34 St 2 MECO
		T+5:35 St 2 sep
		T+5:40 St 3 MES
		T+5:44 Fairing sep
	0159	T+9:38 St 3 MECO
	0159	T+9:54 St 3 sep	158 x 212 x 51.6
	0200	Adapter sep
	0302	T+1:13:45 DM MES-1
	0309	T+1:20:22 DM MECO-1
	0822	T+6:32:57 DM MES-2
2001 Jun 16			631.79 202 x 35821 x 51.6
	0824	T+6:34:56 DM MECO-2
	0844	T+6:54:56 DM sep
2001 Jun 16			783.28 7709 x 35829 x 16.0
2001 Jun 19		LAM-1	890.82 12760 x 35819 x 9.9
2001 Jun 20		LAM-2	1220.08 27061 x 35827 x 2.3
2001 Jun 22		LAM-3	1366.33 32987 x 35832 x 0.6
2001 Jun 24		LAM-4	1397.14 32888 x 35796 x 0.4
2001 Jun 25		LAM-5	1436.56 35777 x 35814 x 0.1 GEO 32.6E+0.1W
2001 Jul 18			1436.09 35764 x 35809 x 0.0 GEO 32.5E
2001 Jul 20		mv out
2001 Aug 3			1438.19 35819 x 35835 x 0.0 GEO 24.2E+0.5W
2001 Aug 29		Move into GEO	1436.09 35768 x 35804 x 0.1 GEO 19.1E
2006 Jul 28			1436.13 35766 x 35807 x 0.1 GEO 19.3E

Into the Black : JPL and the American Space Program, 1976-2004

 https://welib.org/md5/81f4ee4509ea6ef3b6b98135223ec65a

The Times complete history of the world : the ultimate work of historical reference

 https://welib.org/md5/419d07565c7768cb32a69729c51a049e