Intelsat 902

 2001-039A

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SS/Loral FS-1300 Extended satellite. Launch by Ariane 4. (also 903, 904). Mass 4723 kg. At 60.0E Dry mass 1978 kg. Size 2.8 x 3.5 x 5.6m with 31m span.

Intelsat 902
Date	Time	Event	Orbit
2001 Aug 30	0646	Launch by Ariane 44L	CSG ELA2
		T+2:30 PAL sep
		T+3:31 St 1 sep
		T+3:34 St 2 MES
		T+4:22 Fairing sep
		T+5:43 St 2 sep
	0651	T+5:48 St 3 MES
	0704	T+18:42 St 3 MECO
	0706	T+20:49 St 3 sep
		T+21:00 St 3 avoidance maneuver
2001 Aug 30			630.97 179 x 35801 x 7.0
2001 Sep 1	1200	LAM-1
2001 Sep 2	0845	LAM-2	1201.86 26368 x 35765 x 0.7
2001 Sep 4	1540	LAM-3	1435.60 35757 x 35796 x 0.1 GEO 56.5E+0.1E
2001 Oct 20			1436.09 35760 x 35812 x 0.1 GEO 62.0E
2002 Jan 15			1436.06 35773 x 35798 x 0.0 GEO 62.0E
2006 Aug 3			1436.08 35774 x 35797 x 0.0 GEO 62.0E

Iridium 62

 1998-021A

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Iridium SV62 was launched on the third Iridium Proton mission. 

Iridium 62
Date	Time	Event	Orbit
1998 Apr 7	0213:03	Launch by Proton-K	KB
	0214	Stage 1 sep
	0217	Stage 2 sep
	0217	Fairing sep
	0221	Stage 3 sep	140 x 140 km x 73 ?
	0250:07	T+37:04 DM2 burn 1
	0250:32	T+37:29 DM2 MECO-1
	0333	DM2 burn 2
	0338	DM2 MECO-2
	0341	Iridium deployment begins
	0410?	T+1:57? DM2 MES-3 deorbit
	0438?	T+2:25? DM2 reentry
1998 Apr 7			94.83 498 x 522 x 86.7
1998 Apr 9			94.85 501 x 521 x 86.7
1998 Apr 16			95.76 552 x 558 x 86.7
1998 Apr 18			96.77 601 x 606 x 86.7
1998 Apr 26			100.36 772 x 778 x 86.4
1998 May 3			100.40 777 x 777 x 86.4
2004 Jun 29			100.40 775 x 779 x 86.4
2009 Apr 27			100.40 776 x 779 x 86.4

Town and Country: May 2009

 https://welib.org/md5/ab5b7c365fd252be324b898e7ba9d553

Natural Science in Western History (Complete) (v. 1 & 2)

 https://welib.org/md5/d6fc51b66438cafa1cddbd8e760733b0

Malory's Contemporary Audience: The Social Reading of Romance in Late Medieval England

 https://welib.org/md5/eea0aebde1f1834680efd6f2b8f8107f

Cloudsat

 2006-016A

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An ESSP with a BCP RS-2000. Launch by Delta 7420-10 with Calipso under a DPAF fairing.

Size 2.5 x 2.3 x 2.0 m mass 848 kg full (773 kg dry?). 5.1m span. Cloudsat flies in formation with Picasso-Cena and carry a 94 GHz nadir-looking radar. Both satellites will also fly in looser formation with Aqua as part of the A-Train Constellation: Aqua, Cloudsat, CALIPSO, PARASOL and Aura. Combined launch mass 1295 kg.

Orbit 717 x 734 x 98.08. A-Train 1:31PM.

Joint NASA/Canada. Carries a cloud profile radar. an IR O2 spectrometer, and a visible imager. It uses the data from the Picasso lidar in combination with its own radar. Launch 2003.

Ground control by RSC/Kirtland, using AFSCN; mission management by JPL.

Now STP P00-4 SMC-801, Cloud and Aerosol Vertical Profiler.

Calipso is mounted on the upper DPAF cone-cylinder. The lower DPAF cone remains attached to the Delta second stage.

Cloudsat
Date	Time	Event	Orbit
2006 Apr 28	1002:16	Launch by Delta 7420-10C
		T+1:04 SRM 1-4 out
		T+1:22 SRM 1-4 sep 29 km
		T+4:24 MECO 112 km
		T+4:40 SES-1
		T+4:45 Fairing sep
	1013:32	T+11:16 SECO-1	173 x 684 x 98.1
	1102:16	T+1:00:00 SES-2 12s
		T+1:00:12 SECO-2
	1104:18	T+1:02:02 Calipso sep 690 km
	1137:31	T+1:35:15 Upper DPAF sep
	1138:51	T+1:36:35 Cloudsat sep
2007 Jul 4		burn to adjust orbital lifetime

Payload:

• PASBI Profiling A-band Spectrometer/Visible Imager 7500A, 1.3mu

• CPR Cloud Profiling Radar, mm-wave radar

• Propulsion system, 200m/s capability mono hydrazine, 4 x 4.5N, Isp 220s

USA-181

 2004-050A

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The HLV-OLDSP Heavy Lift Vehicle Operational Launch Service Demonstration Payload (DemoSat) is a 5993 kg 1.95m high x 1.38m dia cylindrical test payload to record launch environment.

The Delta IVH has three LOX/LH2 RS-68 powered CBC stages in tandem and a 5-m D4HSS and 5m fairing. The vehicle is 71.6m tall and has a launch mass of 720t. Cargo capacity is 23t to LEO. Launch thrust is 8700 kN. This was the first flight of the 5-meter diameter upper stage. The CBCs cut off 8s early leading to long SES-1 and SES-2 burns, and the second stage ran out of fuel in the third burn. The post-SECO-1 orbit was marginal, with an apogee of around 105 km,

The Demosat carried USAF-STP's University Nanosat-2, two separating payloads built by ASU and UCoBoulder and integrated by AFRL/VS, and was to have tested low shock satellite separation systems. The satellites were dispensed afte SECO-1 and reentered in less than one orbit.

Delta 4H
Date	Time	Event	Orbit
2004 Dec 21	2150:00	Launch	SLC37B
		T+0:50 Center RS-68 to 57 percent thrust
		T+3:55 Outboard RS-68 to 57 percent
		T+4:00 Outboard CBCs MECO (8s early?)
		T+4:08 Outboard CBCs sep 75 km
		T+4:08? Center RS-68 to 102 percent
		T+4:50? 101 km
		T+5:30 Center CBC MECO 149 km
	2155	CBC sep
	2155:53	T+5:53 RL10B-2 SES-1 129 km
	2156:03	T+6:03 5-m fairing sep 134 km
	2203:17?	RL10B-2 SECO-1
	2206:52	T+16:52 Nanosat stack sep in low orbit	105 x 196 km
	2210:29	T+20:29 RL10B-2 SES-2
	2218:32	T+28:32 RL10B-2 SECO-2	185 x 35788 x 27
			645.30 288 x 36428 x 27.2
	2235	Nanosats at 120 km
	2246?	Nanosat perigee?
2004 Dec 22	0327:13	T+5:37:13 RL10B-2 SES-3
	0330:28	T+5:40:28 RL10B-2 SECO-3
	0339:37	T+5:49:37 Demosat sep
	0345:45	T+5:55:45 CCAM
		T+5:57:55 CCAM end
2005 Jan 7			1044.67 19032 x 36420 x 13.5

Optus C1

 2003-028B

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Optus C1/D will also carry a military payload for the Australian Defense Force. Contractor is Mitsubishi Electric with a Space Systems/Loral bus. Launch to 156E. Mass 4725 kg. Box + 2 cruciform panels. dry is 1978 kg, 8.2 x 7.8 x 24.9m deployed. Owner is Singtel Optus Pty (formerly Cable and Wireless Optus Ltd (CWO)), Sydney. Control from CWO/Belrose.

Optus C1 was on an 1194H adapter. The 5.2m Sylda E (+300mm) adapter was used, with a medium fairing with one 0.5m model 5400 extension shell.

Optus C1/D
Date	Time	Event	Orbit
2003 Jun 11	2238:15	Launch by Ariane 5G	CSG ELA3
		T+2:22 EAP sep
		T+3:20 Fairing sep
		T+9:45 EPC MECO
	2248:07	T+9:52 EPC sep	55 x 1972 x 7.5
	2248:14	T+9:59 EPS MES
	2305:07	T+26:52 EPS MECO
	2306:22	T+28:07 Optus sep from 1194H adapter
	2310:14	T+31:59 Sylda 5E sep
	2313:17	T+35:02 BSAT 2 sep from 937V5 adapter
		T+51:21 end of V161 mission
2003 Jun 12	0005?	EPC reentry
2003 Jun 12			637.42 604 x 35707 x 7.03
2003 Jun 14		LAM-1	926.83 14600 x 35621 x 1.8
2003 Jun 16	0130?	LAM-2
2003 Jun 18			1403.73 34687 x 35613 x 0.04 GEO 143E+8E/d
2003 Jul 8		GEO 151E
2003 Jul 12		GEO 156E
2006 Aug 8			1436.10 35772 x 35800 x 0.0 GEO 156.0E

Superbird 4

 2000-012A

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Space Communications Corp of Tokyo ordered an HS-601HP in 1998. HS-601HP Superbird 4 launch by Ariane in 2000. Operational position 162E. The satellite was known as Superbird B2 when in operation.

Launch mass is 4057 kg. Dry mass is 1657 kg. Size is 2.8 x 2.3 x 2.6 m with 26m span.

Superbird 4
Date	Time	Event	Orbit
2000 Feb 18	0104	Launch by Ariane 44LP V127	CSG ELA2
		T+1:09 PAP sep
		T+2:27 PAL sep
		T+3:32 St 1 sep
		T+3:33 St 2 burn
		T+4:37 Fairing 01 sep
		T+5:44 St 2 sep
		T+5:48 St 3 burn
	0122	T+18:51 St 3 MECO
	0125	T+21:09 St 3 sep
2000 Feb 18			630.76 223 x 35747 x 5.0
2000 Feb 22?		LAM-1
2000 Feb 22			857.45 11282 x 35755 x 1.9
2000 Feb 26?		LAM-2
2000 Feb 29			1436.19 35777 x 35799 x 0.1 GEO 139.2E
2000 Mar 30		mv out
2000 Apr 18			1436.07 35774 x 35797 x 0.1 GEO 162.3E
2000 May 27			1436.07 35773 x 35798 x 0.1 GEO 162.4E
2006 Aug 4			1436.09 35784 x 35788 x 0.0 GEO 162.0E

Talent

https://welib.org/md5/b8cdf6280b5af39d1f4d72ae7b29ffbd

March 8,2001

 https://web.archive.org/web/20080504032246/http://digest-archive.degrassi.ca/DD126.htm

The Luxe

 https://welib.org/md5/69d3dcd941670d591f447e85ee6068c5