GOES-7

 1987-022A

---

Geostationary Operational Environmental Satellite 07 (GOES H) was launched by Delta 3914 from Cape Canaveral at 2305 on 1987 Feb 26. The Delta second stage entered a 21 degree parking orbit, separated and executed a depletion burn, ending up in a 252 x 3904 km x 21.7 deg orbit. Meanwhile the Star 37E third stage fired to enter a 284 x 40835 km x 18.1 deg transfer orbit. GOES 7 separated and at 1746 on Feb 27 fired its solid motor to enter a drift orbit at geostationary altitude. The archival orbital data is a little inconsistent; an element set which matches this burn was issued with the printed TLEs but is no longer in the public archive. Assuming it is correct, another burn was made on Mar 1 which lowered the orbit to only a 1343 min period, below the geostationary ring, before another burn raised it again to 1380 min on Mar 2. By Mar 5 it was on station at 81.5 deg W for checkout. By Apr 10 it had taken up GOES E duties at 75W, giving a two satellite GOES system for the first time since 1984. In early 1989 it moved to 108W. From Jul to Oct of 1989, 1990 and 1991 it was moved to 98W for a better view of the hurricane season. In Jan 1992 it was moved to 112W, arriving in Apr 1992. In 1998 the satellite was left to drift; and in the 2000s it was transferred to PEACESAT for Pacific Island communications.

GOES 7
Date	Time	Event	Orbit
1987 Feb 26	2305	Launch by Delta 3924	CC
	2309	Stage 2 burn
	2309	T+4:25 Fairing, 84 km
	2315?	Stage 2 SECO-1	185? x 232 x 28.77
	2325?	Stage 2 burn 2
	2325?	SECO-2
		Spinup
	2326?	Stage 2 sep
	2327?	Star 37E burn at equator crossing
	2328?	Star 37E burnout
	2329?	Star 37E sep	733.32 281 x 40836 x 18.1
		Stage 2 depletion	128.97 252 x 3904 x 21.7
1987 Feb 27	1746	Star 27 burn over 106W?
1987 Feb 27		(old elset)	1455.87 31664 x 40680 x 0.5 GEO 111.8W+4.9W
1987 Feb 27	1756?	Star 27 eject
1987 Mar 1	1950?	Lower orbit
1987 Mar 1			1343.82 31839 x 36082 x 0.6 GEO 118.4W+24.8E
1987 Mar 2	1730?	Orbit raise
1987 Mar 2			1382.10 33362 x 36083 x 0.6 GEO 95.8W+14.1E
1987 Mar 6			1437.16 35579 x 36035 x 0.6 GEO 82.4W+0.2W
1987 Apr 3			1435.94 35763 x 35803 x 0.5 GEO 75.4W
1987 May 3			1436.07 35760 x 35812 x 0.4 GEO 74.5W
1988 Oct 15			1436.27 35739 x 35840 x 0.0 GEO 74.9W+0.05W
1988 Nov		mv to 108W	1436.42 35760 x 35826 x 0.1 -0.1/d
1989 Jan 5		mv in	1436.10 35766 x 35808 x 0.0 GEO 82.0W
1989 Jan 25		mv out	144.0.17 35854 x 35878 x 0.1 GEO 81.3W+1.0W
1989 Mar 19		mv in	1436.08 35780 x 35792 x 0.0 GEO 108.7W
1989 Jul 21			1436.13 35776 x 35798 x 0.0 GEO 107.3W
1989 Jul		Move to 98W
1989 Jul 28			1436.08 35767 x 35804 x 0.1 GEO 97.9W
1989 Oct 10			1436.10 35766 x 35806 x 0.0 GEO 97.5W
1989 Oct 27		mv out
1989 Dec 19		mv in	1436.16 35771 x 35804 x 0.0 GEO 107.4W
1990 Apr 28			1435.76 35758 x 35801 x 0.1 GEO 107.3W
1990 May 1		mv out
1990 Jul 3			1435.84 35757 x 35805 x 0.1 GEO 100.3W+0.06E
1990 Sep 13		mv in	1436.03 35767 x 35803 x 0.1 GEO 97.5W
1990 Oct 18			1437.17 35794 x 35820 x 0.0 GEO 97.1W
1990 Oct 18		mv out
1990 Nov 30			1437.07 35445 x 36165 x 0.1 GEO 108.2W+0.2W
1990 Dec 9		mv in	1436.08 35765 x 35807 x 0.0 GEO 107.6W
1991 May 29			1436.09 35778 x 35794 x 0.1 GEO 107.3W
1991 May 31		mv out
1991 Aug 1		mv in	1435.86 35473 x 36090 x 0.0 GEO 99.1W
1991 Oct 3			1436.05 35776 x 35794 x 0.0 GEO 97.1W
1991 Oct 21		mv out
1992 Jan 16		mv in	1436.30 35776 x 35804 x 0.1 GEO 108.9W+0.06W
1992 Feb		Drift to 111W
1992 Mar 27			1436.18 35770 x 35806 x 0.0 GEO 111.0W
1992 Jul 3			1436.10 35780 x 35793 x 0.0 GEO 111.1W
1992 Dec 10			1436.08 35723 x 35848 x 0.0 GEO 111.0W
1992 Dec		Move to 112W
1992 Dec 19			1436.15 35779 x 35796 x 0.3 GEO 112.2W
1993 Apr 13			1436.06 35767 x 35804 x 0.6 GEO 112.3W
1994 Jan 30			1436.06 35773 x 35798 x 1.3 GEO 112.4W
1994 Dec 20			1436.12 35779 x 35794 x 1.9 GEO 112.2W
1994 Dec 21		mv out	1438.49 35826 x 35840 x 2.0
1995 Feb		mv in
1995 Feb 10			1436.35 35779 x 35803 x 2.1 GEO 135.4W
1995 Dec 1		GOES W	GEO 135.3W
1995 Dec 31			1435.93 35778 x 35788 x 2.7 GEO 134.7W
1996 Jan		Replaced by GOES 9
1996 Jan 26		mv out of GEO
1996 Jul 10		mv in	GEO 95W
1996 Jul 30			1436.10 35762 x 35810 x 3.1 GEO 94.3W
1996 Nov 18			1435.97 35602 x 35965 x 3.3 GEO 95.1W
1997 Apr 30			1436.26 35769 x 35810 x 3.7 GEO 96.0W
1997 Jul 5			1436.35 35782 x 35800 x 3.8 GEO 99.7W
1998 Jan 16			1436.20 35775 x 35801 x 4.2 GEO 98.8W
1998 Jan 31		attitude control tests
1998 Oct 1			1436.27 35783 x 35796 x 4.7 GEO 99.4W
1998 Nov 16			1436.32 35781 x 35800 x 4.7 GEO 101.7W+0.06W
1999 Jun 14			1436.21 35780 x 35797 x 5.1 GEO 112.9W+0.04W
1999 Jun		Relocate to Pacific as PEACESAT
2002 Sep 28			1436.05 35765 x 35805 x 7.3 GEO 177.7W
2003 Jul 5			1435.76 35755 x 35804 x 7.9 GEO 177.7W
2004 Jan 6			1436.06 35778 x 35793 x 8.2 GEO 176.2W
2004 Apr 22			1435.53 35758 x 35792 x 8.4 GEO 170.8W+0.1E

Progress M-52

 2005-007A

---

Spacecraft 11F615A55 No. 352 on mission 17P. Included the PCE (Proximity Communications Equipment) to be installed on ISS for the ESA ATV.

Mass 7259 kg launch, 6966 kg docking.

 

Progress M-52
Date	Time	Event	Orbit
2005 Feb 28	1909:18	Launch by Soyuz-U No. 093	KB LC1/5
		T+1:59 Strapon sep
		T+2:41 GO sep
		T+4:47 Blok A Sep
		T+4:57 KhO sep
	1918:03	T+8:45 MECO
	1918:07	T+8:49 sep
2005 Mar 1	0051	DV1 17m/s
	0137	DV2 8m/s
	1954	DV3
2005 Mar 2	1817:33	DV 24 m/s
	1842:45	DV 1 m/s
	1903:31	DV 25 m/s
	1945	DV 8.8m/s
	1950	Begin flyaround
	1951:42	5 m/s, at 1 km
	1954	2m/s, 550 m
	1959	Stationkeep at 160m
	2002	Resume approach
	2010:08	Docked with Zvezda
	2019:10	DV 0.7m/s 15s
2005 Jun 15	2016:10	Undock
	2316:00	Deorbit 85.8m/s 162.1s	347 x 353 x 51.6
	2319:12	DO CO	56 x 353 x 51.6
	2351:27	Entry

Cosmos 1

 2005-F02

---

Orbital launch Volna late 2001. Built by NPOL/Babakin. 850 x 850 km orbit. 8 blades, 600 m2 aluminized mylar.

Mass 103 kg on orbit (23 kg sail) with 8 15-m petals, spanning 30m. Petals are 5 micron aluminized Mylar polyethlteraphtalate, inflated with nitrogen. Expected solar thrust is 5mN.

Has nosecone: blunt cone 1.1d 1.75l TPS Apogee motor 0.42d 0.50?l Isaev liquid engine UDMH/N2O4, 240s burn giving 0.9?km/s.

S/C 1.1l 1.1d cone-cylinder-cone (two cones connected by small cylinder); deployed 28.8d with 8 blades.

Control from Babakin/Moskva.

Cosmos sail
Date	Time	Event	Orbit
2005 Jun 21	1946:09	Volna launch from Borisoglebsk
		Stage 1 sep
		Stage 2 sep
		Stage 3 burn
	1952:27	T+6:18 Stage 3 sep	-2000? x 765 x 80
		T+15 min telemetry starts
	2005:22	T+19:13 Apogee engine burn
		AKM sep	832 x 840 x 78.6
		Plume shield sep (planned)
		Spinup to 95 rpm (planned)
		Solar sail deploy(planned)
	2007	T+21 min loss of telemetry
		Spindown
	2019?	Reentry?

Payload:

• 8-bladed solar sail

• UHF, S-band radio systems

• Advanced Pixel Sensor CMOS camera

• CCD rotating Matrix camera (Mars-96 model)

• Microaccelerometers

• Charged particle environment monitor

Navstar 61

 2004-045A

---

GPS IIR-13 was launched in Nov 2004 after some hurricane-related delays.

GPS SVN 61
Date	Time	Event	Orbit
2004 Nov 6	0539:00?	Launch by Delta 7925-9.5	CC SLC17B
		T+1:06 SRM 1-6 jett 18 km 1.011 km/s	-6330? x 20? x 36.9
	0541	T+2:01 SRM 7-9 jett 52 km 2.468 km/s	-6050? x 70? x 36.9
	0543	T+4:23 MECO 111 km 6.020 km/s	-3700? x 150? x 36.9
		T+4:31 St 1 sep
		T+4:37 SES-1 119 km 6.021 km/s	-3700? x 150? x 36.9
	0543:58	T+4:58 Fairing sep 130 km 6.079 km/s	-3600? x 165? x 36.9
	0549:54	T+10:54 SECO-1 176 km 7.862 km/s	174 x 393 x 36.90
	0558:55	T+19:55 SES-2 195 km
	0559:31	T+20:31 SECO-2	191 x 1270 x 37.2
	0600:24	T+21:24 Stage 2 sep
	0601:01	T+22:01 TES
	0602:27	T+23:27 TECO
	0604:21	T+25:21 Stage 3 sep	173 x 20371 x 39.1
	0604:23	T+25:23 Yo-yo weights sep
	0729	T+1:50:00 SES-3 depletion
	0729	T+1:50:23 SECO-3	172 x 1293 x 33.1
2004 Nov 9			159 x 20380 x 39.1
2004 Nov 9	0240?	AKM burn
2004 Nov 11			19794 x 20486 x 54.8

Star Trek: Strange new worlds VI

 https://welib.org/md5/680354a84daac687aa5d5c3bc4efa25d

Progress M-51

 2004-051A

---

Spacecraft 351, Mission 16P. Mass 7268 kg launch, 6912 kg at docking. Undocking mass 5655 kg.

The ship carried ROKVISS, a German-built robot arm (Robotic Components Verification on ISS) which will be EVA-mounted externally.

Biorisk may also have been carried.

After undocking Progress was used for tests of microgravity attitude control regimes.

PM51
Date	Time	Event	Orbit
2004 Dec 23	2219:34	Launch by Soyuz-U Zh15000-092	KB LC1
		T+1:58 strapon sep
		T+2:41 GO sep
		T+4:47 Blok A sep
		T+4:57 KhO sep
		T+9:45 MECO
	2228:24	T+9:49 Blok I sep
2004 Dec 24	0205:41	DV1 21.2m/s 53s
	0643:21	DV2 16.9m/s 43s
2004 Dec 24	2344:21	DV3 1.3m/s 5s
2004 Dec 25	2133:35	14m/s 38s range 339 km
	2217:56	18m/s 47s range 104 km
	2259:01	8m/s range 2.4 km
	2307:53	2m/s range 600m
	2319	Range 160m
2004 Dec 25	2358	Docked with Zvezda
2005 Feb 21			91.71 355 x 361 x 51.6
2005 Feb 27	1606:30	Undocked from Zvezda	91.70 355 x 360 x 51.6
	1609:30	0.7 m/s sep
	1908:00	Lower perigee 11m/s	91.28 317 x 357 x 51.6
2005 Mar 9	1617:00	Deorbit burn 152s 79.7 m/s 48.2N 59.5E	315 x 354 x 51.6
	1619:32?	DO cutoff 51.0N 73.5E	46 x 354 x 51.6
	1620:02	DO cutoff
	1652:12	Entry

Seventeen: March 2005

 https://welib.org/md5/3f52b991499abb0bb834880ff851d4c5

TSL: the Droids (songs and members)

 Core members, who began the band in 1990

Dana Larson, vocals & keyboardist

Max Dellon, bass

Dan Scott, bass

Emily Mayer, drums

Guy Chesney, guitarist

Lynne Henry, vocals

Added in 1991

Julie Porter, pianist

Carter Rollins, synthesizer 

Grace Oliver, vocals

Theresa Lyman, vocals 

Thomas Josephs, keyboardist 

Jennifer Mitchell, rhythm guitarist

Added in 1992

Andrea Slade, electric guitarist

Johanna Porter, vocals

Born with a Mike (1992,commercial release 1995)

Dana Larson,vocals

Emily Mayer,keyboard,backing vocals

Max Dellon,bass,backing vocals

Julie Porter,piano,backing vocals

Guy Chesney,keyboard

Grace Oliver,synthesizing keyboard

Lynne Henry,backing vocals

Johanna Porter,backing vocals

Aline Montgomery,music video director

Music video extras:

Mary Judson

Rachel Grant

Michelle Accette

Rosie Shaw

Cammi Adams

Tessa Campanelli

Lacey Frells

Nikki Darling

Cara Walker

Maria Slater

Christine Nelson

Lois Waller

Annie Whitman

Alexa Pappadopolos

Chloe Murphy

Suzanne Hanlon

Bethel McCoy

Brooke Dennis

Caitlin Ryan

Jeannie West

Heather Mallone

Heather Sanford

Toni Jennings

 

Xanadu (1992,commercial release 1995)

Larke Tanner,vocals

Dana Larson,backing vocals

Johanna Porter,backing vocals

Julie Porter,piano,synthesizer

Max Dellon,vocals,bass

Tim Bradley,backup bass

Aline Montgomery,music video

Mary Judson,video work

Aaron Dallas,video work

You Already Know (cover) (1993,commercial release 1994)

Dana Larson,main vocals

Grace Oliver,backing vocals

Emily Mayer,drums and backing vocals

Julie Porter,keyboard

Guy Chesney,keyboard

Aline Montgomery,music video director

 

Couples shown in music video (ordered by appearance):

Elizabeth Wakefield and Todd Wilkins

Cara Walker and Winston Egbert 

Peggy Abbott and John Pfeiffer

Lila Fowler and Christian Gorman

Julie Porter and Bruce Patman

Sandra Bacon and Jeannie West

Caitlin Ryan and Joey Jeremiah 

Guy Chesney and Lynne Henry

Cammi Adams and Jeff Schafer

Emily Mayer and Dan Scott

Dana Larson and Max Dellon

Kerry Glenn and Tad Johnson

Raduga 5

 1979-035A

---

Raduga No. 15 was launched in Apr 1979 to the 85E Statsionar 1/3 slot.

Raduga No. 15
Date	Time	Event	Orbit
1979 Apr 25	0344	Launch by Proton-K	KB
	0353	Stage 3 sep
	0501?	DM burn 1
	1017?	DM burn 2
	1021?	DM sep
1979 Apr 30			1436.49 35794 x 35794 x 0.4 GEO 84.3E-0.1W
1979 May			GEO 85E
1979 Jun 4			1436.06 35750 x 35821 x 0.3 GEO 85.5E
1980 Feb 21			1436.13 35727 x 35847 x 0.2 GEO 85.3E
1980 Jul			GEO 85E
1981 Aug			GEO 87E
1981 Dec 20			1436.23 35754 x 35823 x 1.6 GEO 85.3E+0.04W
1982 Jan			GEO 83E
1982 Apr			GEO 86E
1982 May 27		mv out
1987 Jul 22		drifting	1436.28 35765 x 35815 x 6.6 GEO 84.0E+0.05W

Town and Country: March 2005

 https://welib.org/md5/6bdd45e9f8686798fb57f4b40010e9b7

Kosmos 2410

 2004-038A

---

A satellite launched in Sep 2004 was reported to be a test of a new model developed by the Arsenal/Progress team. It would have a life of 6 months. After only 107 days the spacecraft was deorbited but the capsule was lost.

The spacecraft may be designated 11F695U Kobal't-M, or Yantar'-4K2M / Kobal't-1.

One day before recovery two objects were ejected into 169 x 248 km x 67 deg orbits; they reentered within a day.

Kosmos-2410
Date	Time	Event	Orbit
2004 Sep 24	1650	Launch by Soyuz-U	PL LC16
	1654	Blok A sep
	1659	Blok I MECO
	1659	Blok I sep
	2250		89.75 165 x 358 x 67.1
2004 Sep 29	2046		89.38 161 x 325 x 67.1
2004 Oct 1	1151		89.23 159 x 312 x 67.1
	1732		89.95 213 x 330 x 67.1
2004 Oct 15	1217		89.61 206 x 304 x 67.2
2004 Nov 1		SpK-1 fiducial
	0358?	Deorbit
	0420?	Land
2004 Dec 1		SpK-2 fiducial
	1839?	Deorbit
	1901?	Land
2004 Dec 9			205 x 335 x 67.1
2005 Jan 1			190 x 317 x 67.1
2005 Jan 8		C,D ejected
2005 Jan 9	0330		183 x 288 x 67.1
	0410	Pass over 98E 44N rev 1709
	0540	Pass over 75E 44N rev 1710
2005 Jan 9	0728?	Deorbited after 107d
	0742?	Entry
	0753?	Landed?
	0710	Pass over 54E 46N rev 1711
	0840	Pass over 32E 46N rev 1712

The Complete Book of Spaceflight

https://welib.org/md5/7c52df7572369adaeb515be9dd2577af

AMC-11

 2004-017A

---

A2100 satellite, mass 2315 kg. To replace Satcom C-3, working with AMC-10. Box + 2 panels.

AMC 11
Date	Time	Event	Orbit
2004 May 19	2222	Launch by Atlas IIAS AC-166	CC SLC36B
		T+0:59 SRM 3-4 on
		T+1:12 SRM 1-2 sep
		T+1:56 SRM 3-4 sep
		T+2:42 BECO
		T+2:45 Booster sep
		T+3:25 Fairing sep
		T+5:06 SECO
		Atlas sep
		T+5:25 MES-1
	2231	T+9:37 MECO-1
		T+23:56 MES-2 1:56
	2247	T+25:53 MECO-2	186 x 35926 x 12.4
	2250	T+28:13 Centaur sep
2004 May 20			629.53 176 x 35730 x 12.5
2004 May 22	0800?	LAM-1
2004 May 23			1196.83 26219 x 35705 x 0.9
2004 May 24	2000?	LAM-2
2004 May 25			1433.55 35717 x 35755 x 0.1 GEO 147.8W+0.6E
2004 Jun 3			1436.10 35779 x 35794 x 0.0 GEO 146.0W
2004 Oct 16		Relocate from 146W to 131W
2004 Oct 30			1436.01 35779 x 35790 x 0.1 GEO 131.0W

FSW-20

 2004-039A

---

On landing, the recovery capsule fell through the roof of a house in Tianbeizi.

FSW
Date	Time	Event	Orbit
2004 Sep 27	0800	Launch by CZ-2D	JQ
	0810?	CZ-2D sep
2004 Sep 27			89.53 205 x 297 x 63.0
2004 Sep 28	0740	Orbit raise	89.77 206 x 320 x 63.0
2004 Oct 4			89.76 205 x 319 x 63.0
2004 Oct 4		Orbit raise	89.80 206 x 323 x 63.0
2004 Oct 7			89.80 205 x 322 x 63.0
2004 Oct 15			89.71 203 x 317 x 63.0
	0226?	SRV separate
		SRV deorbit	-400? x 530? x 63.0
	0248	SRV landed