Kosmos 1696

 1985-095A

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Two-tone telemetry; Hi res satellite

Kosmos-1696
Date	Time	Event	Orbit
1985 Oct 16	0925	Launch by Soyuz	KB
	0929	Blok I burn
	0933	Blok I MECO
1985 Oct 16			89.31 207 x 272 x 70.4
1985 Oct 17	0020?	Raise orbit	89.62 229 x 281 x 70.4
1985 Oct 23			89.59 228 x 279 x 70.4
1985 Oct 28			89.57 227 x 277 x 70.4
1985 Oct 30
	0611?	Deorbit
	0623?	PO sep
	0630?	Entry	-179 x 251 x 70.4
	0645?	Landed

Kosmos 1312

 1981-098A

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Kosmos-1312
Date	Time	Event	Orbit
1981 Sep 30	0800	Launch by 11K68	PL
		T+2:00 St 1 sep
		T+3:33 GO sep
		T+4:38 St 2 sep, alt 148 km	-2700? x 200? x 82.6
		T+5:20 S5M burn 1, alt 172 km	-2700? x 200? x 82.6
	0806	T+6:52 S5M MECO-1, alt 222 km	-31 x 1502 x 82.6
		T+42:18 BOZ burn
		T+43:56 S5M MES2	-31 x 1502 x 82.6
		T+44:15 S5M MECO2
	0844	T+44:45 S5M sep
1981 Sep 30			1492x1503x82.59

Gambit-3 7

 1967-079A

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KH-8 7 (GAMBIT 4307) was launched on 1967 Aug 16 by Titan 3B Agena D from Vandenberg. Perigee was 148.7 km, 11 km higher than planned due to a 7,6m/s overspeed. By rev 31 the perigee had decayed to 147.8 km and an orbit adjust reduced this to 139 km. The roll joint locked up initially but was freed after four hours.

KH-8 7
Date	Time	Event	Orbit
1967 Aug 16	1707	Launch by Titan IIIB Agena D	V SLC4W
	1712	Agena burn
	1717	MECO	90.4 142 x 449 x 111.9
1967 Aug 17	0742		90.42 143 x 446 x 111.9
		Rev 31 Perigee lower
	1644		90.38 140 x 446 x 111.6
1967 Aug 21	2030?	Rev 81, TCM2
1967 Aug 26	2130?	Rev 162, TCM3
1967 Aug 26	2306?	SRV rev 163
1967 Aug 27	1031		89.39 122 x 365 x 111.6
1967 Aug 28	2250?	Deboost rev 195

Kosmos 1806

 1986-098A

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Kosmos-1806 transmitted until early 1990. At times it provided communications support for the third long-duration Mir expedition.

Kosmos-1806
Date	Time	Event	Orbit
1986 Dec 12	1835:36	Launch by 8K78M	Plesetsk
		BVGD sep
		GO sep
		T+4:46 Blok A sep
		T+4:56 KhO sep
		T+8:46 Blok-I MECO
	1844	T+8:50 Blok-I sep
		T+1:00? BOZ burn
	1936?	T+1:00? BOZ sep
		2BL burn
		2BL MECO
	1939?	T+1:03 2BL sep
1986 Dec 12			(98B) 92.3 217x557x62.8
1986 Dec 12			(98C) 205x606x62.8
1986 Dec 12			(98D) 706.0 618x39152x62.8
1987 Feb 20			706.7 614x39140x62.8

Yuri 2A

 1984-005A

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NASDA managed the BS-2 program for Japan's first operational direct broadcast service operated by NHK (Nihon Hoso Kyokai). The satellite, built by Toshiba and GE had a mass of 350 kg on orbit. Two transponders malfunctioned so only one channel was available.

The spacecraft was a box 1.3 x 1.2 x 1.5m. Used 26 kg dry, 321 kg prop, 1.24m l 0.69m dia Star 27 motor for insertion.

Yuri 2A
Date	Time	Event	Orbit
1984 Jan 23	0758	Launch by N-2	TNSC
		T+0:38 SRM sep
		T+4:33 MECO
		T+4:42 Stage 1 sep
		T+4:52 SES-1 6:26
	0803?	T+5:02? Fairing sep
	0809	T+11:18 SECO-1	197 x 197? x 30.0?
	0821	T+23:08 SES-2
	0821	T+23:18 SECO-2	110.26 197 x 2296 x 30.0
	0823	T+25m Stage 2 sep
	0823	T+25m Stage 3 burn 43s
	0824	TECO, Transfer orbit injection
	0825	Stage 3 sep
	1400?	Apo 1
	1900?	Peri 1
1984 Jan 24	0030?	Apo 2
	0530?	Peri 2
	1100?	Apo 3
	1600?	Peri 3
	2200?	Apo 4 over 170W
1984 Jan 25	0245?	Peri 4
	0800?	Apo 5
	1300?	Peri 5
	1800?	Apo 6 over 126W
1984 Jan 25			635.46 200 x 36011 x 28.4
1984 Jan 26
	0000?	Peri 6
	0500?	Apo 7 over 73E
1984 Jan 26	0514	Star 27 burn at apo 7
		Despin using thrusters
		Solar arrays deployed
	1030?	Peri 7
	1600?	Apo 8 over 87W
1984 Jan 26			1431.14 35359 x 36020 x 0.4 GEO 152.1E+1.2E
1984 Jan 29	0230	Orbit adjust
1984 Feb 15		On station 110E
1984 Feb 26			1436.10 35784 x 35788 x 0.3 GEO 110.0E
1985 Jul 14			1436.07 35783 x 35788 x 0.1 GEO 110.0E
1985 Oct 17			1436.17 35776 x 35799 x 0.1 GEO 110.0E
1985 Nov		move to 108E
1985 Nov 22			1436.12 35780 x 35793 x 0.1 GEO 108.1E
1986 Mar 12			1436.16 35783 x 35792 x 0.0 GEO 108.0E
1987 Feb 7		mv out	1436.17 35784 x 35791 x 0.0 GEO 107.8E+0.03W
1987 Mar 5		mv in	1436.16 35779 x 35796 x 0.0 GEO 109.9E
1987 Jul 20			1436.09 35777 x 35795 x 0.1 GEO 110.0E
1988 Sep 9			1436.17 35774 x 35802 x 0.2 GEO 109.7E
1988 Nov 4			1436.09 35761 x 35811 x 0.4 GEO 110.2E