Panamsat 1

 1988-051C

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Pan American Satellite of Greenwich, Connecticut, bought the ASC 3 satellite from GE Astro Space. The company later was renamed Alpha Lyracom and then Panamsat, Inc.

PAS 1
Date	Time	Event	Orbit
1988 Jun 15	1119:01	Launch by Ariane 4	CSG ELA2
		T+1:06 PAP sep 7 km
		T+2:29 PAL sep 39 km, Vi 1.75km/s	-6250 x 60?
		Stage 1 sep T+3:32 75 km Vi 3.238km/s	-5900 x 150?
		T+3:37s St 2 MES
		Fairing sep T+4:46 115 km Vi 4.317km/s	-5300 x 200?
	1124	Stage 2 sep T+5:45 148 km Vi 5.884 km/s	-3950 x 300?
		T+5:50 St 3 MES
	1137	M+0, T+17:43 Stage 3 MECO
	1139	M+2:12 T+19:55 Meteosat sep
	1139	M+2:17 T+20:00 Cyclade Adapter sep from SPELDA
	1140	M+3:30 T+21:13 SPELDA Adapter sep
	1142	M+5:16 T+22:59? PAS 1 sep
	1145	M+8:51 Stage 3 evasion burn
	1239	AMSAT sep from Cyclade
	1700?	Apo 1
	2200?	Peri 1
1988 Jun 16	0400?	Apo 2 over 75W
	0900?	Peri 2
	1500?	Apo 3 over 125E
	1930?	Peri 3
1988 Jun 17	0100?	Apo 4 over 35W
1988 Jun 17	0118?	Star 30C burn
1988 Jun 19			1441.20 35611 x 36161 x 0.1 GEO 41.1W+1.3W
1988 Jul 12		mv in	1436.09 35782 x 35791 x 0.0 GEO 45.2W
1989 Jan 11			1436.15 35779 x 35796 x 0.0 GEO 45.1W
1992 Jan 1			1436.15 35772 x 35804 x 0.0 GEO 45.0W
1993 Dec 22			1436.16 35782 x 35792 x 0.0 GEO 45.0W
1996 Jun 14			1436.13 35772 x 35802 x 0.0 GEO 45.0W

Polyot 2

  1964-019A

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The second launch of the 11A59/Polyot system came in Apr 1964. This time only the final orbit was announced initially. Object 783 (1964-19B) in a 238 x 497 km x 60.0 deg orbit, reentered after 18 days. Object 784 (1964-19A) in a 302 x 479 km x 58.1 deg orbit, stayed in orbit until 1966.

Polyot-2
Date	Time	Event	Orbit
1964 Apr 12	0930	Launch by 11A59	KB
		T+1:30 strapon thrust reduced
	0932	T+2:05 8K74BVGD strapon sep
		Fairing sep
	0935	T+5:30 8K74A core burnout, sep	-500? x 300? x 58.0?
1964 Apr 12	0940?	T+10:30? Polyot engine burn
	0942?	Polyot engine cutoff	242 x 485 x 59.92
		Second burn failed
1964 Apr 13	0211	(19B)	91.90 238 x 497 x 59.95
1964 Apr 13	1607	(19A)	92.38 302 x 479 x 58.05
1964 Apr 15?		End of transmissions?
1964 Apr 17		(19B)	91.54 236 x 463 x 59.92
1964 Apr 22		(19A)	92.37 304 x 476 x 58.06
1964 May 8		(19B) reentered
1966 Jun 8	2110?	(19A) reentered

Reference Books Bulletin 1994-95: A Compilation of Evaluations September 1994, Through August 1995

 https://welib.org/md5/2d5f2c391052d568b0886deb9f6ef089

DSP 12

 1984-129A

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DSP 6R was refurbished and launched in Dec 1984 as a Phase II Upgrade satellite. It had a new primary sensor, the SED, and a MWIR for observing smaller missiles. The SED had 6000 pixels on the focal plane and included above-the-horizon capability. 

DSP 6R
Date	Time	Event	Orbit
1984 Dec 22	0002:03	Launch by Titan 34D/Transtage	CC LC40
	0004?	SRM sep
	0006?	Stage 1 sep
	0007?	Fairing
	0009?	Stage 2 MECO
	0010?	Stage 2 sep (129C, d Jan 17)
	0100?	Transtage MES-1
	0630?	MES-2
	0630?	MECO-2
	0700?	Transtage sep
1984 Dec 23?		Cover sep
1984 Dec			1445.8 35915 x 36190 x 3.4
1985 Mar			GEO 155W
1985 May 25		Opl WPAC	GEO 155W
1988 May 20		mv out	GEO 155W
1988 Jul 1		drift	GEO 90E
1988 Jul 20			GEO 65E
1991 Jun 15		mv out	GEO 65E
1991 Jul 10			GEO 145E
1992 Aug 20		mv out	GEO 145E
1992 Sep 2		mv in	GEO 105E
1993 Jun 15		mv out	GEO 105E
1993 Jul 20		mv in	GEO 5E