All Eyes On Her

 https://welib.org/md5/dd41904490d2d89e1d4dbeece816934d

The Best of the Best : Becoming Elite at an American Boarding School

 https://welib.org/md5/75c73a19b663a4315e74fbe11e806118

Turksat 1C

 1996-040B

---

Turksat 1C was lauched by Ariane for Aerospatiale, which delivered it on orbit to Turk Telecom. Launch mass was 1743 kg, BOL mass 1078 kg and dry mass 789 kg. The satellite is 1.64 x 1.46 m x 2.20 m with a 22.20 m span. It was built by Aerospatiale-Cannes. The satellite was launched in the lower Ariane position, underneath the SMS (Stretched Mini Spelda) structure. It provides services to Turkey. Initial test position is 31.3E, then service position is 42E.

Turksat 1C
Date	Time	Event	Orbit
1996 Jul 9	2224	Launch by Ariane 44L (V88)	CSG ELA2
	2227	Stage 1 sep T+3:32
	2229	Stage 2 sep T+5:43
	2229	Stage 3 TIG T+5:48
	2242	Stage 3 MECO T+18:45
	2244	Arabsat 2A sep T+20:00
	2246	SMS sep T+22:52
	2248	Turksat sep T+24:20
1996 Jul 11			630.00 212 x 35718 x 7.0
1996 Jul 11	1130?	LAM-1
1996 Jul 11			755.49 6476 x 35722 x 3.4
1996 Jul 12	1230?	LAM-2
1996 Jul 12			1299.66 30345 x 35798 x 0.2
1996 Jul 14	0730?	LAM-3
1996 Jul 14			1434.18 35688 x 35810 x 0.1 GEO 29.9E+0.5E
1996 Jul 20			1435.81 35775 x35786 x 0.1 GEO 31.4E
1996 Jul 22			GEO 31.3E+0.1/d
1996 Aug 6			1436.02 35773 x 35796 x 0.1 GEO 31.3E
1996 Sep 14			1436.00 35769 x 35799 x 0.0 GEO 31.5E
1996 Sep		Move to 42E
1996 Oct 4			1436.07 35773 x 35799 x 0.0 GEO 42.0E
1999 Oct 15			1436.09 35777 x 35795 x 0.0 GEO 42.0E
2006 Aug 1			1436.06 35768 x 35803 x 0.1 GEO 42.0E
2008 Jul 30		GEO 42E, move to 30E
2008 Aug 24			1436.03 35772 x 35798 x 0.4 GEO 31.0E
2010 Jan 29			1436.08 35771 x 35800 x 2.2 GEO 31.0E

December 29,1998

 https://web.archive.org/web/20080504033425/http://digest-archive.degrassi.ca/DD53.htm

January 2000

https://web.archive.org/web/20080504034040/http://digest-archive.degrassi.ca/DD76.htm

https://web.archive.org/web/20080504034054/http://digest-archive.degrassi.ca/DD78.htm

https://web.archive.org/web/20080504034816/http://digest-archive.degrassi.ca/DD80.htm

https://web.archive.org/web/20080504034823/http://digest-archive.degrassi.ca/DD81.htm

https://web.archive.org/web/20080504034830/http://digest-archive.degrassi.ca/DD82.htm

ST-5

 2006-008A

---

Each Nanosat Constellation Trailblazer is 25 kg, 0.52m dia 0.48 high oct prism with an extendable boom for 1.0m? span. Three satellites on a single launch to 300 x 4500 km x 97 deg on Pegasus XL from Vandenberg. Built by GSFC. Will study magnetosphere; spacecraft highly magnetically clean to allow short mag booms.

ST5
Date	Time	Event	Orbit
2006 Mar 14	1327	L1011 T/O V RW30/12
	1428	Abort
	1448s	Land on RW12
2006 Mar 22	1304	L1011 T/O V RW30/12
	1403:45	Drop
	1403:50	T+0:05 Stage 1 on 70s
	1405:02	T+1:17 Stage 1 burnout
		Stage 1 sep
	1405:16	T+1:31 Stage 2 on
	1405:55	T+2:10 Fairing sep, 115 km
	1406:29	T+2:44 St 2 burnout, 156 km
	1409:02	T+5:17 Stage 2 sep
	1409:02	T+5:17 Stage 3 burn 283 km
	1410:09?	T+6:24? Stage 3 burnout
	1413:16s	T+9:31 ST5-FWD sep S+0
	1416:26	T+12:41 ST5-2 sep S+200s
	1419:36	T+15:51 ST5-3 sep S+390s	301 x 4568 x 105.6
		Pegasus CCAM
	1532		298 x 4554 x 105.6
2008 Jun 30		end of ops

Payload:

• X-band transponder, Aero Astro comms system

• CULPRIT Low power microelectronic device, CMOS ultra low power radiation tolerant logic.

• Cold gas microthruster, Fine attitude adjustment

• Lithium ion power system

• Magnetometer booms, 0.36m long

Disney High School Musical 3: Hats Off, Wildcats!: A Graduation Guide from Your Favorite Seniors

 https://welib.org/md5/8b59355daeb5b89267d804a3c81cf39d

Kosmos 2459

 2010-007A

---

Kosmos-2459/2460/2461 or Glonass 731 732, 735 in block 40. Launch by Proton 53540 and DM-2 No 116L.

K2459
Date	Time	Event	Orbit
2010 Mar 1	2119:44	Launch
	2129:30	St 3 sep
	2155:59	DM-2 MES-1
	2202:15	DM-2 MECO-1
2010 Mar 2
	0049:02	DM2 MES2
	0051:36	DM2 MECO2
	0051:51	DM2 sep from Glonass

Haiyang 3

 2011-043A

---

Ocean No. 2 (Haiyang er hao) with CZ-4B. Orbit was 689 x 712 km x 88 deg.

HY2
Date	Time	Event	Orbit
2011 Aug 15	2257	Launch by CZ-4B	TYSC
	2259?	St 1 sep
	2300?	Fairing sep
	2303?	St 2 MECO
	2303?	St 2 sep
		St 3 burn
	2307?	St 3 MECO
	2317?	St 3 sep

Payload:

• MWI Microwave imager, for brightness temp

• RA Dual band radar altimeter C/Ku, sea levels and wind speeds

Seeing further : the story of science, discovery, and the genius of the Royal Society

 https://welib.org/md5/261e3a121c0b6f31e02d5c37701e0128

Koreasat 6

 2010-070B

---

Korea Telecom satellite built by Thales as prime contractor with an Orbital Star-2 bus. Mass 2750 kg launch. Size 4.3 x 2.3 x 3.2m with 18m span. Mass 2850 kg launch 1150 kg dry. Location at 116E for Korean domestic comms.

Koreasat 6
Date	Time	Event	Orbit
2010 Dec 29	2127	Launch by Ariane 5
		T+2:13 EAP sep
		T+3:02 Fairing sep
	2135	T+8:49 EPC MECO
		T+8:55 EPC sep
	2136	T+8:59 ESC-A burn
	2151	T+24:55 ESC-A MECO
	2154	T+27:20 Hispasat sep
	2156	T+29:39 Sylda sep
	2201	T+34:05 Koreasat 6 sep
2011 Dec 29			632.17 268 x 35774 x 3.0
2011 Jan 1			717.72 4592 x 35759 x 2.3
2011 Jan 3			1036.04 19311 x 35765 x 0.9
2011 Jan 5			1260.41 28775 x 35771 x 0.2
2011 Jan 8			1434.53 35731 x 35780 x 0.1 GEO 117.8E+0.3E/d
2011 Jan 18			1436.16 35782 x 35783 x 0.0 GEO 118.4E

Beidou 8

 2010-024A

---

4th Beidou navigation satellite, or COMPASS G3.

DW4
Date	Time	Event	Orbit
2010 Jun 2	1553:04	Launch by CZ-3C Y4
		T+2:07? Booster sep
		T+2:27? St 1 sep
		T+3:52? Fairing sep
		T+5:32? St 2 sep
		T+5:32? St 3 MES-1
	1603	T+10:31? MECO-1	210? x 450? x 28.5?
	1614	T+21:21? MES-2
	1617	T+24:20? MECO-2
	1619?	Stage 3 sep	205 x 35647 x 20.5
2010 Jun 4			627.25 203 x 35585 x 20.5
2010 Jun 8			GEO
2010 Jun 14			1436.09 35778 x 35794 x 1.8 GEO 84.7E

Skynet 4D

 1998-002A

---

Skynet 4D is the first of three replacement Skynet 4 Stage 2 satellites. It will be launched 1998 by Delta. It is built by Matra Marconi Space/Stevenage. It still uses the old ECS bus, but has a steerable high power SHF spot beam and widebeam antennae.

During launch, the Delta second stage suffered two jolts, one during the second burn and one 15 s into the depletion burn, which caused the nearly empty stage to tumble.

The Skynet 4D was transferred from MMS to MoD on 1998 May 20.

In early 2003 4D was moved from the Atlantic position to support troops in the Middle East.

Skynet 4D
Date	Time	Event	Orbit
1998 Jan 10	0032:01	Launch by Delta 7925	CC LC17B
	0033:04	SRM 1-6 burnout
	0033:07	SRM 7-9 burn, 1-6 sep
	0034:10	SRM 7-9 burnout, sep
	0036:24	T+4:23 MECO
	0036:32	T+4:31 Stage 1 sep
	0036:38	T+4:37 Stage 2 burn 324s
	0036:48	T+4:47 Fairing sep
	0042:02	T+10:01 SECO 1	165 x 212 x 29.2
	0053:01	T+21:00 Stage 2 restart 37s
	0053:38	T+21:37 SECO 2	340? x 1140? x 28.6
	0139:29	T+1:07:28 Stage 2 restart 41s
	0140:10	T+1:08:09 SECO 3	1085? x 1372? x 28.6
	0141:53	T+1:09:52 Stage 2 sep
	0142:30	T+1:10:29 Stage 3 burn
	0143:57	T+1:11:56 TECO
	0145:50	T+1:13:49 PAM-D sep
	0145:52	Yo-yo deploy
	0202:00	Stage 2 depletion 25s	764 x 1296 x 26.9
	0202:15	Stage 2 tumble
1998 Jan 10			655.23 1186 x 36036 x 23.7
1998 Jan 12	0225?	AKM burn
1998 Jan 13			1442.75 35690 x 36143 x 4.2 GEO 43.2W+1.6W
1998 Jan 24			1426.77 35560 x 35647 x 4.2 GEO 24.0W+2.3E
1998 Mar 5			1435.96 35753 x 35814 x 4.2 GEO 6.0E
1998 Apr 21			1436.07 35771 x 35800 x 4.0 GEO 6.0E
1998 Apr		Move out
1998 May 5			1430.85 35545 x 35822 x 4.0 GEO 28.7E+1.3E
1998 May 20		Transfer to MoD
1998 Jul 11	Move in	1436.07 35783 x 35788 x 3.9 GEO 53.0E
1999 Jul 28			1436.05 35782 x 35788 x 3.3 GEO 52.9E
1999 Aug 6		move out
1999 Oct 15			1439.78 35781 x 35935 x 3.1 GEO 34.4W+0.9W
1999 Nov 18			1436.12 35779 x 35794 x 3.1 GEO 33.9W
2000 Oct 4			1436.11 35783 x 35789 x 2.5 GEO 34.0W
2002 Oct 26			1436.11 35780 x 35792 x 1.4 GEO 33.9W
2002 Nov 21			1430.52 35559 x 35795 x 1.4
2003 Jan 31		mv in	1436.20 35777 x 35796 x 1.3 GEO 38.9E
2003 Dec 2			1436.02 35779 x 35791 x 1.4 GEO 39.1E
2003 Dec		Move out of GEO
2004 Mar		mv in	1436.16 35775 x 35800 x 1.5 GEO 34.1W
2004 Aug 11			1436.09 35774 x 35799 x 1.7 GEO 34.1W
2006 Jul 30			1436.18 35781 x 35795 x 3.1 GEO 34.4W

UARS

 1991-063B

---

The Upper Atmosphere Research Satellite, built by General Electric, used the Fairchild MMS bus (like Landsat D). It had a total mass of 6526 kg at deployment per the SODB; 6540 kg per the press kit. The satellite was launched on STS-48. The RMS grappled the satellite at 2300 on Sep 14, and it was finally deployed at 0423:02 on Sep 15 into a 563 x 574 km x 57.0 deg orbit. Orbit raising burns were made at 1035 on Sep 17 and 1036 on Sep 18.

UARS
Date	Time	Event	Orbit
1991 Sep 14	2300	RMS grapple UARS
1991 Sep 15	0423:02	RMS deploy UARS
1991 Sep 15			563 x 574 x 57.0
1991 Sep 17			563 x 574 x 57.0
1991 Sep 17	1035	orbit raise	555 x 587 x 57.0
1991 Sep 18	1036	orbit raise	574 x 575 x 57.0
1991 Sep 24	0230		574 x 581 x 57.0
1991 Sep 30	1200		574 x 581 x 57.0
1992 Jul		ISAMS failed
1993 May		CLAES cryogen depleted
1999?		End of orbit maintenance
2005 Sep 17			550 x 560 x 57.0
2005 Sep 22?		Begin perigee lower
2005 Oct 5		Burn	507 x 558 x 57.0
2005 Oct 6		Burn	473 x 556 x 57.0
2005 Oct 12		Burn	442 x 555 x 57.0
2005 Oct 18		Burn	415 x 554 x 57.0
2005 Dec 8		Burn
2005 Dec 14	1716	decommissioned
2011 Sep 24	0400	Entry over Pacific 14.1S 170.2W

Payload:

• MMS HPM MMS Hydrazine Propulsion Module, 4 x 5lb thrusters

• MMS MACS MMS Modular Attitude Control System. This unit originally flew on Solar Max, and was returned to Earth by Shuttle Mission 41-C in 1984 for refurbishment.

• SUSIM 2 Solar UV spectral irradiance monitor; 1000-4000A solar spectrum. 2 spectrometers in one instrument.

• CLAES Cryogenic Limb Array Etalon Spectrometer

• ISAMS Improved Stratospheric and mesospheric sounder

• MLS Microwave Limb Sounder, 1.6m reflector, 63, 183 and 205 GHz

Seventeen: April 2011

 https://welib.org/md5/7ba7ad67fa7f22c6203cb5fffbed6c3c

Nahuel 1A

 1997-002B

---

Nahuel is an DASA (Dornier Satellitensystemen) Spacebus 2000 satellite for Argentina to provide TV, telephone and data comms for Latin America. Launch mass was 1790 kg; 1100 kg BOL, 831 kg dry. Bus is 1.64 x 1.46 x 2.2m with 22.2 m span. The satellite owner/operator is Nahuelsat S.A. of Buenos Aires, whose largest shareholder at launch time was GE Americom. Nahuel is Araucano for tiger.

Nahuel 1A
Date	Time	Event	Orbit
1997 Jan 30	2204	Launch by Ariane 44L	CSG ELA2
	2206	Stage 1 sep
	2208	Fairing 01 sep T+4:17
	2209	Stage 2 sep T+5:43
	2222	Stage 3 cutoff T+18:45
	2224	GE 2 sep T+20:38
	2226	Mini Spelda sep T+22:18
	2228	Nahuel 1A sep T+24:29
	2228	H10-3 sep burn T+24:33
1997 Jan 31			632.34 203 x 35848 x 7.0
1997 Feb 1	1100?	LAM-1
1997 Feb 1			916.81 13890 x 35876 x 1.9
1997 Feb 2	1750?	LAM-2
1997 Feb 2			1342.06 31947 x 35902 x 0.2
1997 Feb 4	1430?	LAM-3
1997 Feb 4			1431.52 35494 x 35899 x 0.1 GEO 75.0W+1.1E
1997 Feb 6			1437.10 35714 x 35898 x 0.1 GEO 72.5W+0.2W
1997 Feb 10			1436.02 35776 x 35793 x 0.1 GEO 72.2W
1997 Mar 22			1436.08 35770 x 35801 x 0.0 GEO 71.8W
1999 Oct 15			1436.09 35771 x 35801 x 0.0 GEO 71.8W
2006 Aug 3			1436.12 35768 x 35805 x 0.1 GEO 71.8W
2010 Apr 5			1436.13 35768 x 35805 x 2.5 GEO 71.8W
2010 Apr 8		Move out
2010 Apr 12			1436.46 35778 x 35808 x 2.5 GEO 72.5W+0.1W/d
2010 May 12			1436.60 35780 x 35812 x 2.6 GEO 75.8W+0.13W/d
2010 Jun 28			1437.24 35785 x 35932 x 2.7
2010 Jul 15		Orbit raised, retired
2010 Aug 21			1448.86 36007 x 36064 x 2.8
2011 Jun 10			1448.93 36006 x 36067 x 3.5

The Heart of the Wedding

 https://welib.org/md5/7381acefa622e8991d14dcc0ac17056d

February 2,1999

 https://web.archive.org/web/20080504033543/http://digest-archive.degrassi.ca/DD56.htm

Envy (Luxe Series, Book 3)

 https://welib.org/md5/f74e3ced96977bf5b8aba1c898ca8321

Eutelsat W3A

 2004-008A

---

Launched by Proton-M 535-03 with Briz-M 88507. (NK0308-29).

Astrium Eurostar 3000S colocated with W3 at 7W. Provides multimedia and high speed internet. 

Eutelsat W3A
Date	Time	Event	Orbit
2004 Mar 15	2306:00	Launch by Proton-M	KB PL81/24
		T+2:02 St 1 sep
		T+5:27 St 2 sep
		T+5:38 Fairing sep
	2315	T+9:41 St 3 sep	-936 x 163 x 51.5
	2317	T+11:16 Briz MES-1 0.377 km/s
	2324	T+18:21 MECO-1	173 x 173 x 51.5
2004 Mar 16	0014	T+1:08:39 MES-2 1.024 km/s
	0030	T+1:24:42 MECO-2	250 x 5000 x 50.3
	0235	T+3:29:31 MES-3
	0246	T+3:40:13 MECO-3
	0247?	Torus tank jettison	284.29 302 x 15585 x 49.5
	0248	T+3:42:09 MES-4 1.534 km/s
	0252	T+3:46:57 MECO-4	380 x 35814 x 49.1
	0758	T+8:52:10 MES-5 1.143 km/s
	0805	T+8:59:03 MECO-5
	0816	T+9:10:40 Briz sep	701.83 3842 x 35723 x 12.7
	1020	T+11:14:15 MES-6 sep 70 m/s
2004 Mar 17			701.84 3842 x 35723 x 12.7
2004 Mar 22			1428.04 35472 x 35785 x 0.0 GEO 7.0W+2E
2004 Apr 3			1436.10 35777 x 35795 x 0.0 GEO 1.65E
2004 May 15		Move in at 7E
2004 May 23			1436.09 35743 x 35829 x 0.1 GEO 7.0E