Panamsat 2

 1994-040A

---

Panamsat Corp.'s second satellite was an HS-601 model, providing hybrid C/Ku band communications. The 2290 kg PanAmSat K1 (PAS 2) satellite was launched in 1994 aboard an Ariane to become the Pacific region PAS satellite.

PAS 2
Date	Time	Event	Orbit
1994 Jul 8	2305	Launch by Ariane 4 V65	CSG
	2308	T+3:14? Stage 1 sep
	2309	T+4:07? Fairing sep
	2310	T+5:27? Stage 2 sep
	2310	T+5:32? Stage 3 burn
	2323	Stage 3 MECO
	2325?	Stage 3 sep
1994 Jul 8			632.08 243 x 35793 x 7.0
1994 Jul 10	0150?	LAM-1
1994 Jul 10			795.81 8446 x 35690 x 2.9
1994 Jul 11	0410?	LAM-2
1994 Jul 11			1246.10 28260 x 35700 x 0.4
1994 Jul 12	2200?	LAM-3
1994 Jul 13			1393.72 34233 x 35673 x 0.1
1994 Jul 15			1436.34 35645 x 35936 x 0.0 GEO 165.0W
1994 Jul 29			1436.00 35635 x 35934 x 0.0 GEO 164.9W
1994 Jul 31		mv out
1994 Sep 13		mv in
1994 Sep 23			1436.08 35774 x 35798 x 0.0 GEO 169.0E
1995 Aug 19			1436.07 35775 x 35796 x 0.0 GEO 169.0E
1997 May			GEO 191W
1998 Feb 14			1436.07 35763 x 35808 x 0.0 GEO 169.0E
1999 Oct 15			1436.07 35755 x 35816 x 0.0 GEO 169.1E
2006 Aug 2			1436.08 35775 x 35797 x 0.0 GEO 169.0E

NOAA-16

 2000-055A

---

NOAA L was launched by Titan II. Launch mass is 2231 kg including the Star 37. Dry mass is 1475 kg. Size is 4.2l 1.9d with 6.1m long solar array. Deployed length with array about 7.0m.

Standard Star 37XFP is 955 kg full, 72 kg empty. Assmue loaded to only 756 kg. Then reconcile mass as 828 kg f 72 kg dry Star 37 case, 1403 kg ATN bus. 

Orbit is 1358:40LT.

NOAA L
Date	Time	Event	Orbit
2000 Sep 21	1022:04	Launch by Titan II G-13	V SLC4W
		T+2:29 St 1 MECO
		T+2:30 St 1 sep
		T+2:31 St 2 MES, St 1 sep
		T+3:38 Fairing
		T+5:33 St 2 MECO
	1028:41	T+6:37 St 2 sep	-2500 x 850 x 98.8
		T+6:40 End sep burn
	1037	T+15:01.5 Star 37XFP burn
	1037	T+15:52.5 Star 37XFP burnout
	1038:00	T+15:58 Velocity trim 22s
		T+16:19 End trim
	1038:25	Orbit injection
		T+18:17 N2H4 blowdown start
		T+20:37 N2H4 blowdown stop
		T+20:37 solar array mast deploy	848 x 863 x 98.8
	1051	Stage 2 reentry
	1052:16	T+30:16 Sunshade deploy
	1056	Orbit mode handover
		Thruster firings due to AKM chuff
2000 Sep 21		Spacecraft bus active
		AVHRR Vis chan on
2000 Sep 22		AMSU-B on
2000 Sep 24		SARR on
2000 Sep 26		AMSU-A1 /A2 on
2000 Sep 29		Handed over to NOAA
2000 Oct 10		HIRS cooler door open
2000 Oct 11		AVHRR cooler door open
2000 Dec 24			102.05 847 x 864 x 98.8
2001 Mar 20		Replaced NOAA 14 as primary afternoon sat
2006 Aug		PM Secondary

Exploring the Unknown: Selected Documents in the History of the U.S. Civil Space Program, Volume III: Using Space

 https://welib.org/md5/66a3a87d47f894383884dd843e4ad20a

August 23,1998

 https://web.archive.org/web/20080504032848/http://digest-archive.degrassi.ca/DD37.htm

740 Park : The Story of the World's Richest Apartment Building

https://welib.org/md5/2b0bebca57835b6eca444c6c2e116759

Space Exploration: Triumphs And Tragedies

 https://welib.org/md5/a05bb47c98e6b181658242a2d0b8e5f4

Aviation Week: October 15,2007

 https://welib.org/md5/732128cbb99c626adc52b0a63502db65

Telstar 8

 2005-022A

---

IA-8, formerly Loral Skynet Telstar 8, is a 5493 kg FS-1300S (or 1300E?), first extended bus satellite. Total of 92 transponders. Launch by Zenit-3SL. Sold to Intelsat prior to launch in 2003. In 2007 it was renamed Galaxy 28.

IA8
Date	Time	Event	Orbit
2005 Jun 23	1402:59	Launch by Zenit-3SL No. 14	Odyssey
		T+2:29 St 1 sep
		T+3:41 PLF sep
		T+8:35 St 2 sep	-2138 x 179 x 0
		T+8:45 DM MES-1
	1422:24	T+19:25 DM MECO-1	144 x 35609 x 0.1
	1432:14	T+29:15 DM sep
			202 x 35636 x 0 (RKKE)
2005 Jun 24			627.85 165 x 35651 x 0.0
2005 Jun 24	0600?	LAM-1	1150.49 24248 x 35558 x 0.1
2005 Jun 28	0345?	LAM-2	1380.86 33762 x 35634 x 0.17
2005 Jun 29			1426.82 35542 x 35667 x 0.02
2005 Jul 11			1436.10 35766 x 35806 x 0.0 GEO 89.0W
2006 Aug 8			1436.11 35782 x 35791 x 0.0 GEO 89.0W

Space and Astronomy

 https://welib.org/md5/045a8518efd5754bd350c162bbe8ba7f

Telecom 2C

 1995-067A

---

Telecom 2C was the third Eurostar class payload for France Telecom. Launch mass was 2283 kg, BOL mass was 1360 kg, and dry mass was 1120 kg. The bus was 1.9 x 2.6m across and 3.1 m high, with a 22m solar panel span.

Telecom 2C
Date	Time	Event	Orbit
1995 Dec 6	2323	Launch by Ariane 44P (V81)	CSG ELA2
	2326	Stage 1 sep
	2326	Stage 2 on
	2327	Fairing 01 sep
	2328	Stage 2 off (T+5:42)
	2328	Stage 3 on (T+5:48)
	2340	H-10-III cutoff (T+17:06)
	2344	Telecom 2C sep from Mini-Spelda (T+21:18)	630.1 224 x 35712 x 6.8
1995 Dec 7			630.11 223 x 35677 x 7.0
1995 Dec 17			629.42 223 x 35677 x 7.0
1995 Dec 18?		LAM burn
1995 Dec 20?		LAM burn
1995 Dec 21			1435.91 35765 x 35800 x 0.1 GEO 1.0E+0.04E
1995 Dec 24			1436.02 35777 x 35793 x 0.1 GEO 1.0E
1996 Jan 18		mv out
1996 Jan 26		mv in 3E
1996 Feb 18			1436.09 35767 x 35805 x 0.0 GEO 3.0E
1998 Oct 23			1436.05 35771 x 35799 x 0.0 GEO 3.0E
2001 Feb 7			1436.04 35768 x 35802 x 0.1 GEO 3.1E
2007 Jul 24			1436.08 35763 x 35808 x 2.5 GEO 3.1E

Aviation Week: November 19,2007

 https://welib.org/md5/8c62490d7378176cf0a57d9fd8f900f5

MultiMedia & Internet @ Schools: September-October 2007

 https://welib.org/md5/c5de56045a1a816e71ab03e3efdf1e6d

Foton 2005

 2005-020A

---

Launch mass 6425 kg (TsENKI says 6535 kg). Total internal payload mass 382 kg.

Foton M-2
Date	Time	Event	Orbit
2005 May 31	1200:00	Launch by Soyuz-U Zh15000-091	KB LC1/5
		T+1:58 Strapon sep
		T+2:36 GO sep
		T+4:47 Blok A sep
		T+4:50 KhO sep
		T+8:46 Blok I MECO
	1208:49	T+8:49 Blok I sep	258 x 291 x 63.0
2005 Jun 16
	0705	T+15.6d Deorbit burn 137m/s	248 x 276 x 63.0
		Deorbit complete	-220 x 268 x 63.0
	0715?	Battery and PO sep
	0729	Parachute system deploy
	0736	SA landing 52N 64E 140 km SE Kustanai

Payload:

• ESA TCA Tether Cutter Assembly (on battery pack)

• Fluidpac, fluid physics

• Telesupport

• Biopan, 9 exobio and radiation exposure expts

• SCCO diffusion effects on crude oil

• AGAT diffusion coeffs in alloys

• Stone - 2 0.5 kg meteoritic entry expts

• Outreach - 3 edu expts.

• Aquacells - bio, aquatic microorgs, DLR

• Polizon - KBOM crystal growth

• Keramik DLR entry expt.

• Favorite Life support electrolysis test

• DataLogger, ESA/TsSKB Foton environment monitoring

• TAS-3 Triax accelerometer

Gorizont 31

 1996-005A

---

The penultimate Gorizont satellite was launched in Jan 1996 to 40 deg E for testing. It moved to 102E in 2002 and 140E the following year.

Gorizont (31)
Date	Time	Event	Orbit
1996 Jan 25	0956:00	Launch by Proton-K/DM2	KB
	1005	8S812 burn, orbit insertion	88.30 186 x 195 x 51.63
	1100?	Blok-DM2 burn 1
	1620?	Blok-DM2 burn 2
	1640?	Blok-DM2 sep	1482.58 36573 x 36810 x 1.51
1996 Jan 27			1482.58 36573 x 36810 x 1.5 GEO 94.4E+11.3W
1996 Jan 30	1700		1448.26 35907 x 36141 x 1.63
1996 Feb 2	1619		1436.41 35763 x 35822 x 1.52 GEO 40E
1996 Feb 9			1436.32 35763 x 35818 x 1.5 GEO 40.1E
1997 Oct 18			1436.29 35776 x 35804 x 0.3 GEO 40.2E
1999 Oct 18			1436.24 35779 x 35799 x 1.3 GEO 40.1E
2002 Sep		mv out
2002 Sep		mv in	GEO 102E
2003 Jul 5			1435.96 35780 x 35784 x 4.4 GEO 102.7E
2003 Aug 8?		mv up
2003 Sep 5			1434.33 35719 x 35784 x 4.5
2003 Nov 12		move in at 140E	1436.13 35769 x 35804 x 4.7 GEO 140.2E
2006 May 4			1436.17 35783 x 35792 x 6.9 GEO 140.0E