Navstar 60

 2004-023A

---

SVN 60, flight IIR-12 to replace IIA-16 in plane F slot 4.

GPS IIR-12
Date	Time	Event	Orbit
2004 Jun 23	2254:01	Launch by Delta 7925-9.5	CC LC17B
		T+1:30 SRM 1-6 burnout
		T+1:05 SRM 7-9 on
		T+1:06 SRM 1-6 sep
		T+2:09 SRM 7-9 off
		T+2:11 SRM 7-9 sep
		T+2:20 St 1 dogleg
		T+2:40 St 2 end dogleg
		T+4:23 MECO
		T+4:31 St 1 sep
	2258:38	T+4:37 SES-1
		T+4:43 dogleg
		T+4:53 end dogleg
	2258:49	T+4:48 Fairing sep
	2304:55	T+10:54 SECO-1	175 x 392 x 36.90
	2313:56	T+19:56 SES-2
	2314:32	T+20:31 SECO-2	191 x 1270 x 37.21
	2315:22	T+21:21 spinup
	2315:25	T+21:24 St 2 sep
	2316:02	T+22:01 TES
	2317:28	T+23:27 TECO
	2318:12	T+24:11 NCS blowdown
	2319:04	T+25:03 end NCS blowdown
	2319:22	T+25:21 Stage 3 sep
	2319:24	T+25:23 Stage 3 yo deploy
2004 Jun 24	0044:01	T+1:50:00 SES-3
		T+1:50:23 SECO-3
		T+3:19:24 First apogee	355.79 144 x 20364 x 39.0
2004 Jun 26	0750	AKM	720.08 20107 x 20360 x 55.1
2004 Aug 12			718.01 20089 x 20276 x 55.1

Intelsat 4A6

 1978-035A

---

The final IVA to be launched was F-6, in Mar 1978. It was stationed over the Indian Ocean, and in late 1978 replaced IV F-1 as the IOR Primary satellite.

Intelsat 4A F-6
Date	Time	Event	Orbit
1978 Mar 31	2336:01	Launch by Atlas Centaur	CC LC36
		T+2:20 BECO
		T+2:23 Booster sep
		T+3:05 Insulation panels sep
		T+4:02 SECO
		T+4:09 Atlas sep
		T+4:19 MES-1
		T+4:31 Fairing
	2346	T+10:20 MECO-1 189 km vrel 7.786
1978 Apr 1	0000	T+24:53 MES-2 559 km vrel 7.320
	0001	T+25:29 MECO-2 628 km
	0004	T+28:34 Centaur sep	641.03 549 x 35949 x 21.85 (RAE)
	0011	T+35:34 end blowdown
	0600?	Apo 1 85E
	1600?	Apo 2 71W
1978 Apr 2	0300?	Apo 3 130E
	0230?	AKM (speculative) over 130E
1978 Apr 13			1436.13 35731 x 35843 x 0.3 GEO 154.9E+0.02W
1978 May 25			1446.89 35980 x 36014 x 0.3 GEO 112.7E+2.7W
1978 Jun 8			1447.01 35979 x 36020 x 0.2 GEO 74.6E+2.7W
1978 Jun 22		mv in	1436.13 35773 x 35801 x 0.2 GEO 62.9E
1978 Sep 30			GEO 62.9E
1978 Nov 19		Replaced IV F-1
1979 Jan		IOR Primary	GEO 63E
1980 Nov 12			1435.95 35778 x 35789 x 0.1 GEO 63.8E
1982 Sep 12			1436.21 35778 x 35799 x 0.1 GEO 62.9E
1982 Sep 22		mv out	GEO 63E
1982 Nov 18		mv in	1436.07 35781 x 35791 x 0.1 GEO 174.0E
1982 Dec		POR Primary	GEO 174E
1984 Mar 29			1436.12 35782 x 35791 x 0.0 GEO 173.9E
1985 Aug			GEO 174E
1986 Mar 1			1436.09 35783 x 35790 x 0.3 GEO 174.0E
1986 Mar 13			1436.09 35783 x 35790 x 0.3 GEO 173.9E
1986 Mar 18		mv out	1436.37 35781 x 35802 x 0.3 GEO 173.7E+0.08W
1986 Apr		mv out	GEO 174E
1986 Jun 12		mv in	1436.17 35775 x 35796 x 0.6 GEO 170.1E
1986 Oct 6			GEO 170.0E
1986 Dec 17			1436.01 35774 x 35795 x 1.0 GEO 170.1E
1986 Dec 29		Orbit raise	1438.13 35816 x 35836 x 1.0 GEO 164.0E+0.5W
1987 Aug 12			1437.55 35792 x 35838 x 1.6 GEO 47.1E+0.4W
1989 Mar 31			1437.6 35769 x 35860 x 1.7
1993 Dec 31			1435.2 35739 x 35797 x 7.3
1997 Feb 3			1435.32 35751 x 35791 x 9.3 GEO 16.29E+0.2/d

Spot 1

 1986-019A

---

Matra built the SPOT 1 satellite for CNES, which launched it aboard an Ariane into sun synchronous polar orbit in Feb 1986.

SPOT 1 was deactivated in 1993, but was to be reactivated in Nov 1996 to make up for the loss of SPOT 3. By this time, the on board tape recorders had failed and data had to be recovered by ground station real time passes.

In 2003, with 54 kg of prop remaining, the satellite's perigee was lowered to decrease its orbital life, with decay expected in 2018. First, the orbit was lowered in two burns by 15 km to avoid collision risks with the other SPOT satellites and position apogee over Toulouse; then a series of burns were made at apogee to lower perigee including a large final depletion burn. The resulting orbit had an estimated lifetime of 18 years. SPOT 1 was then decommissioned.

SPOT 1
Date	Time	Event	Orbit
1986 Feb 22	0144:35	Launch by Ariane I	CSG
		T+2:29 Stage 1 sep	-6260? x 75? x 98
		T+4:20 Fairing sep	-5800? x 240? x 98
		T+4:44 St 2 MECO
		T+4:48 Stage 2 sep	-5450? x 320 x 98
		T+4:54 St 3 MES
	0158:39	T+14:04 H8 MECO
	0159:12	T+14:37 SPOT sep
	0202:46	T+18:11 Viking sep
	0205	H8 end of mission
1986 Feb 22		101.42 823 x 828 x 98.8
1986 Nov 14		H8 stage explodes
1990 Sep		In reserve
1992 Mar		Reactivated
1992 Oct		Deactivated
1993 Apr		Reactivated
1993 Jul		Deactivated
1993 Sep			101.41 824 x 825 x 98.71
2003 Nov 6			101.40 824 x 826 x 98.67
2003 Nov 17		Begin 1000s deorbit burns	800 x 826 x 98.7
	1309	350s burn
	1413	696s burn	810 x 812 x 98.7
2003 Nov 19		1000s burn, 5 kg	783 x 808
2003 Nov 20		1000s burn	757 x 808
2003 Nov 21		1000s burn	732 x 807
2003 Nov 22		1000s burn	708 x 807
2003 Nov 24		1000s burn	684 x 806
2003 Nov 25		1000s burn	662 x 805
2003 Nov 26		1000s burn	640 x 804
2003 Nov 27		1000s burn	619 x 804 x 98.7
2003 Nov 28	2023	Depletion 2400s, 8.4 kg
	2103	End of burn
2003 Nov 30		end of ops
2003 Dec 4			98.64 584 x 803 x 98.7
2004 Jul 22			98.63 584 x 801 x 98.7

Payload:

• HRV /Imaging CCD cameras (2) 0.5-0.59,0.61-0.68,0.79-0.89mu 20m resolution

Confessions Of An Heiress

https://welib.org/md5/b92fd6a0e4c1f030259f0ec8bfb43fd3

High School USA TV show

All seasons - 25 episodes 

TV movie (1983)

Season 1 (1984)

1-1. “The News is Love” (January 12,1984)

Cara Ames (Robin Morse), the newest staffer on the Excelsior High student newspaper, is assigned to escort new kid Jamie Kelso (Timothy Hutton) around the school for his first day, and she discovers that she just may have feelings for him.

2-2. “False Possessions” (January 19,1984)

Mr Lambert (John Erwin) is the new sophomore English teacher,and all the girls are unaccountably going gaga for him. Juniors Beth Franklin (Betsy Russell) and Anne-Marie Conklin (Crystal Bernard) team up to find out just what is going on with him, and what they find leads to a major shakeup.....

Note: This episode marked Erwin’s only live-action appearance in any TV show or movie.

3-3. “Glee Club” (January 26,1984)

Candace Casey (Holly Anderson), one of the senior class’ more popular girls, has appointed herself President of the EHS Glee Club, leading to a series of hijinks that keep the club members on their toes, especially junior Jessica Abbott (Nichole McAuley).

4-4. “Caught in a Trap” (February 2,1984)

In this Groundhog Day special, Beau Middleton (Anthony Edwards) finds himself repeating February 1 over and over again until Beth agrees to kiss him.

Note: This episode,according to internal evidence,is meant to take place in February 1981.

5-5. “Anne-Marie on Air” (February 9,1984)

Rebecca Macmillan (Robyn Donny) is the director of the school’s new video service,which would be a good thing if she didn’t have an ongoing rivalry with Anne-Marie,the main correspondent,leading to Becky doing all she can to interfere with Anne-Marie’s show and learning a valuable lesson in the process.

6-6. “Hard Choices” (February 23,1984)

Beth is torn on whether to go to the Valentine Ball with Beau or with kind-hearted J.J.Manners (Neil Patrick Harris). She goes to her mother (Mary Jo Deschanel), whom she’s always trusted on such matters,and her response leads her to choose J.J.

Season 2 (1985)

Season 3 (1986)

Season 4 (1987)

Season 5 (1988)

Reunion movie (2001)

Anik C1

 1985-028B

---

In 1993 Anik C-1 was sold to Paracomsat, owned 90 percent by Paracom SA of Buenos Aires and 10 percent by Telesat. It was moved to 72W to provide Paracom services as a precursor to Argentina's Nahuel system. In 1996 Telesat bought the satellite back since Argentina now had Nahuel 1A. In Apr 2000 Anik C-1 was acquired by Loral Skynet do Brasil and renamed Brasil 1(T). It was then moved to 63W to provide limited service awaiting the launch of Loral's Estrela do Sul satellite.

Anik C-1
Date	Time	Event	Orbit
1985 Apr 12		Launch by Shuttle (51-D)	KSC LC39
1985 Apr 12	2338	Deploy
1985 Apr 13	0023	PAM-D burn 83s
	0024	PAM-D cutoff
	0026	PAM-D sep
1985 Apr 13			626.28 348 x 35390 x 23.00
	0630	Apogee 1 over 118E
	1050	Perigee 1
	1700	Apogee 2 over 38W
	2115	Perigee 2
1985 Apr 14	0320	Apogee 3 over 166E
	0745	Perigee 3
	1340	Apogee 4 over 10E
	1810	Perigee 4
1985 Apr 14	2332?	Star 30B burn at Apogee 5
1985 Apr 15	0010	Apogee 5 over 148W
1985 Apr 14			1407.42 34988 x 35458 x 3.0 GEO 146.2W+7.3E
1985 Apr 16			1422.88 35443 x 35611 x .30 GEO 130.7W+3.3E
1985 Apr 16			1422.9 35441x35618x2.9
1985 Apr 17			1431.36 35627 x 35760 x 2.9 GEO 127.6W+1.2E
1985 Apr 18			1431.1 35618x35762x2.9
1985 Apr 21			1430.9 35618x35759x2.9
1985 May 4		On station	GEO 107.5W
1985 May 5			1436.07 35778 x 35793 x 2.9 GEO 107.5W
1986 Oct 28			1436.10 35774 x 35798 x 1.5 GEO 107.4W
1988 Nov 1			1436.08 35782 x 35790 x 0.0 GEO 107.3W
1990 Apr 5			1436.10 35776 x 35796 x 0.0 GEO 107.3W
1991 Oct 1			1436.10 35778 x 35794 x 0.0 GEO 107.3W
1991 Oct		Move to 110W
1991 Oct 4			1436.07 35775 x 35796 x 0.0 GEO 110.0W
1991 Dec 27			1436.10 35775 x 35797 x 0.0 GEO 109.3W
1993 Feb			GEO 109.3W
1993 Mar 29		mv out
1993 Mar 29		Sold to Paracom SA
1993 Apr 1			1436.07 35775 x 35796 x 0.1 GEO 109.2W
1993 Apr 5			1425.77 35403 x 35764 x 0.1 GEO 91.0W+2.6E
1993 Apr 17			1426.01 35385 x 35791 x 0.1 GEO 65.3W+2.5E
1993 May 5		mv in	1436.06 35781 x 35790 x 0.1 GEO 71.5W
1993 Jun 1		Begin Paracom services as Nahuel A
1993 Sep 12			1436.11 35781 x 35791 x 0.0 GEO 71.8W
1994 Sep 19			1436.18 35781 x 35795 x 0.0 GEO 72.0W
1996 mid		Bought back by Telesat
1996 Nov 22			1436.11 35782 x 35790 x 0.0 GEO 71.8W
1997 Apr			GEO 72W
1997 Apr 11		mv out	1444.50 35929 x 35972 x 0.1 GEO 77.6W+2.1W
1997 May 9		mv in	1436.20 35756 x 35820 x 0.2 GEO 118.6W
1998 Mar 30			1436.02 35771 x 35799 x 0.8 GEO 118.5W
1998 Apr		Drift
1998 May 16			1435.66 35766 x 35789 x 0.9 GEO 115.8W+0.1E
1998 Aug 20		mv in	1436.10 35776 x 35796 x 1.1 GEO 106.3W
1999 Jun 10			1436.09 35776 x 35796 x 1.8 GEO 106.3W
2000 Apr 13			1436.08 35772 x 35800 x 2.4 GEO 106.3W
2000 Apr 14?		mv out
2000 Apr 30			1434.35 35744 x 35760 x 2.5 GEO 99.0W+0.4E
2000 Jul 18			1434.62 35754 x 35760 x 2.6 GEO 66.6W+0.4/d
2000 Aug 1?		Move in at 63W
2000 Aug 3			1435.81 35776 x35785 x 2.7 GEO 63.0W
2000 Sep 2			1436.13 35779x 35794 x 2.7 GEO 63.0W
2003 Apr 24			1436.15 35781 x 35793 x 5.0 GEO 63.3W

Soyuz 9

  1970-041A

---

The Soyuz-9 mission, which used spacecraft 7K-OK No. 17, was a transition mission between the lunar and Salyut phases of the Soyuz program. Andrian Nikolaev and Vitaliy Sevastyanov spent a record 18 days in space. The BO carried a thermal control system prototype for DOS/Almaz.

Sevastyanov said in 2001 that three 0.5-meter target subsatellites were ejected from the BO and tracked optically in support of an Almaz-related space defense experiment. 

Soyuz-9
Date	Time	Event	Orbit
1970 Jun 1	1900:00	Launch by Soyuz	KB
		T+1:55 SAS sep
		T+1:58 Blok BVGD sep
		T+2:45 Fairing
		T+4:48 Blok A sep
		T+4:48 St 3 MES
	1908:50	T+8:50 St 3 MECO
	1909?	St 3 sep
	2315		88.53 176 x 228 x 51.64
1970 Jun 2		3 subsats ejected
	0043	Ascending node at apogee
	0044	Begin rev 5?
1970 Jun 2	0105?	Burn on rev 5
	0212	End of rev 5
	0300	End of working day
	0330		88.59 180 x 225 x 51.64
1970 Jun 3	1230		89.54 244 x 260 x 51.68
1970 Jun 16			89.05 222 x 234 x 51.68
	0930	Orbit lower	88.78 210 x 219 x 51.68
	1645		88.75 199 x 226 x 51.68
1970 Jun 18	1915		88.44 196 x 200 x 51.67
1970 Jun 19	1052	Prep for retrofire
1970 Jun 19	1117:30	Retrofire 145s, 0.15 km/s
	1119:55	DO CO
	1132?	Modules sep
	1140?	Entry
	1144	Parachute deployment
	1158:55	Landed 75 km W of Karaganda

Opera: A History in Documents

https://welib.org/md5/021e21a311460f9855feb81889763e34

We Have Capture

https://welib.org/md5/7ad00281606de66bd1d8b00a706427bc

Kosmos 2407

 2004-028A

---

A Parus satellite was launched in Jul 2004,continuing the annual replenishment.

Kosmos-2407
Date	Time	Event	Orbit
2004 Jul 22	1746:28	Launch by Kosmos-3M	PL LC132/1
	1748	Stage 2 MES-1
	1754?	Stage 2 MECO-1
	1848?	Stage 2 MES-2
	1848?	Stage 2 MECO-2
	1849:30	S3M sep

Kosmos 2406

 2004-021A

---

Kosmos-2406 was launched by FKA in Jun 2004 as the first replenishment launch for Tselina-2 in 4 years.

Kosmos-2406
Date	Time	Event	Orbit
2004 Jun 10	0128:00	Launch by Zenit-2	KB
	0130	T+2:23 St 1 MECO
	0130	T+2:25 Stage 1 sep
	0130	T+2:25 Stage 2 burn
	0130	T+2:40 GO sep
	0134	T+6:42 Stage 2 MECO	150? x 850? x 71.0
		Sep motor cover perigee
	0141?	T+13m? Stage 2 VECO
	0141?	Stage 2 sep motor covers
	0141	T+13m Stage 2 sep
2004 Jun 17			102.05 846 x 865 x 71.0

Ekspress AM-11

 2004-015A

---

AM No. 11 and No. 12 replaced the cancelled Troika/Spacebus-3000 project. These are separate from AM 1-3 and have Alcatel payloads. AM 11 has 26 C and 4 Ku. 2542 kg launch. AM 11 was launched for GP KS by Proton K 410-08 with Blok DM-01 11S861-01 No. 14L.

Ekspress AM-11
Date	Time	Event	Orbit
2004 Apr 26	2037:00	Launch by Proton-K 410-08	KB PL200/39
		T+2:06 St 1 sep
		T+3:03 GO sep
		T+5:33 St 2 sep
		T+9:34 St 3 MECO
	2046	T+9:44 St 3 sep
	2047	T+10:39 DM adapter sep	154 x 155 x 51.6
	2150	T+1:13:27 MES-1
	2157	T+1:20:34 MECO-1	632.51 329 x 35730 x 47.5
2004 Apr 27	0306	T+6:29:24 MES-2, SOZ sep
	0309	T+6:32:41 MECO-2	143.06 35777 x 35794 x 0.0 GEO 96.5E
	0309:57	T+6:32:57 DM sep
2004 Apr 27		R/B reentered
2004 May 19			1436.13 35785 x 35788 x 0.1 GEO 96.5E