Kosmos 2005

 1989-019A

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Kosmos-2005
Date	Time	Event	Orbit
1989 Mar 2	1900	Launch by Soyuz	PL
	1908	Blok-I sep
1989 Mar 3.0			89.65 189x326x62.8
1989 Mar 15			89.64 175x338x62.8 from 88.72 155x267
1989 Mar 21			89.69 176x342x62.8 from 89.20 167x303
1989 Mar 22		SpK-1 fiducial
1989 Mar 26			89.87 180x356x62.8 from 89.19 167x302
1989 Apr 5			89.57 177x329x62.8 from 88.94 168x277
1989 Apr 10			89.84 183x351x62.8 from 88.99 168x282
1989 Apr 12		SpK-2 fiducial
1989 Apr 15			89.45 175x320x62.8 from 89.30 174x307
1989 Apr 20			89.13 178x286x62.8 from 88.80 160x271
1989 Apr 22			88.77 184x243x62.8 from 88.59 166x244
1989 Apr 24			88.67 182x235x62.8
1989 Apr 25
	1940?	Deorbit
	2007?	Landed

Kosmos 1920

 1988-010A

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Resurs F-1 14F40 No. 106 was launched in Feb 1988. Like spacecraft 104, it used the higher 91.2 minute circular orbit, and like spacecraft 107 it completed a 20 day flight.

Kosmos-1920
Date	Time	Event	Orbit
1988 Feb 18	0950	Launch by Soyuz-U	PL LC16
	0958	Blok-I sep	88.74 189 x 236 x 82.6
1988 Feb 20			89.60 180 x 237 x 82.6
1988 Feb 21			91.17 330 x 334 x 82.6
1988 Mar 5			91.16 323 x 341 x 82.6
1988 Mar 9			91.10 318 x 339 x 82.6
	0546?	Deorbit
	0556?	PO sep
	0610?	Entry
	0623?	Landed

Explorer 9

  1961-004

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The second S-56 payload, S-056A, was launched on 1961 Feb 16 by Scout X-1 from Launch Area 3 at Wallops Island. It reached orbit at 1316 and the balloon canister split to begin inflation of the 6 kg, 3.5m diameter balloon. The balloon's radio beacon failed on the first orbit, but the final rocket stage transmitted until 1961 Feb 25. The orbit of Explorer 9 was 634 x 2583 km x 38.9 deg. It reentered on 1964 Apr 3.

Explorer 9
Date	Time	Event	Orbit
1961 Feb 16	1305	Launch by Scout X-1	WI LA3
		T+0:42 St 1 burnout
		T+1:10 St 1 sep
		T+1:10 St 2 burn 40 km
		T+1:51 St 2 burnout
		T+1:56 St 3 burn
		T+1:56 St 2 sep 94 km
		T+1:56 Fairing sep
		T+2:36 St 3 burnout
		T+9:39 St 4 spinup
		T+9:41 St 3 sep
	1314	T+9:42 Stage 4 burn, V = 4.5 km/s dV = 3.0 km/s	-5050? x 641 x 38.8
	1316	T+10:22 Stage 4 burnout 52.5W 35.2N
		T+10:28 Canister opened
		T+10:29 Balloon inflation
	1320	T+14:59 Balloon ejected
	1420	end of balloon transmissions
1961 Feb 25		end of Altair transmissions
			634 x 2583 x 38.9
1964 Apr 3		Reentered

ATS 5

  1969-069A

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ATS E (Applications Technology Satellite 5) was the third successful ATS. Launch by Atlas Centaur was at 1101 UT on 1969 Aug 12. Because of its heavier mass, ATS-5 needed a more elliptical parking orbit and a shorter coast time. The satellite was inserted into geostationary transfer orbit and fired its SR-28-3 apogee motor (serial number was either Z-4 or Z-6). The AKM was fired at first apogee instead of the planned second because of an attitude control anomaly. The apogee motor was to have been ejected 90s later to improve stability characteristics, but the spacecraft went into a flat spin and the ejection was aborted. ATS 5 was allowed to drift into view of the Rosman ground control station, and was maneuvered so that the spin was around the correct axis, but upside down. The motor was jettisoned on Sep 5. It impacted the solar array during ejection and caused minor damage. Because ATS-5 was spinning in the wrong direction, the yo-yo system could not be used and the gravity gradient booms could not be deployed. The spacecraft remained at 105 deg W until 1978 when it was moved to 70W; in 1984 it ran out of stationkeeping fuel and was moved off station. Its orbit was raised sometime in the months following Apr 1984.

ATS 5
Date	Time	Event	Orbit
1969 Aug 12	1101:04	Launch by Atlas Centaur
		T+2:32 BECO
		T+2:35 Booster sep
		T+3:21 panel jettison, 520 kg.
		T+3:53 Fairing sep, 970 kg
		T+4:10 SECO
		T+4:13 Atlas sep
		T+4:23 Centaur burn
	1111	T+10:39 Centaur MECO 25 min coast	142.80 181 x 5158 x 26.79
	1136	T+35:43 Centaur MES2 1:11
	1137	T+36:54 Centaur MECO2	686.46 2147 x 36645 x 17.60 (Delta rpt)
	1140	T+39:09 Centaur sep
		T+46:09 Centaur blowdown, pos-sep burn H2O2, 49s
		T+46:58 Centaur post-sep H2O2 off
		T+46:59 Centaur venting	703.7 2187 x 37471 x 17.59 (AC)
	1150?	ATS-5 spun up to 95 rpm
	1710?	AKM 44s burn	1463.97 35763 x 36901 x 2.7 (PLR No2)
			35784 x 36908 x 2.62
			35688 x 36809 x 2.62 (TMX-2383)
	1710		1416.43 34844 x 35956 x 2.7 GEO 90.5E+5.0W
1969 Aug 12		attitude control issues
1969 Aug 17		attitude control recovered
1969 Sep 5		AKM jettison
1969 Sep 5		Yo-yo despin
1969 Oct 2			1435.99 35778 x 35791 x 2.6 GEO 106.6W
1970 Aug 2			1436.12 35726 x 35847 x 1.7 GEO 104.9W
1971 May 31			1436.22 35724 x 35853 x 1.0 GEO 105.1W
1974 May 3			GEO 105.4W
1975 Sep 17			GEO 104.9W
1976 Mar 15			GEO 104.9W
1977 Jan 10			GEO 105.4W
1977 Feb?		Move out
1977 Feb 18			1434.83 35731 x 35792 x 3.8 GEO 94.8W+0.3W/d
1977 May		Move in
1977 May 25			1435.94 35773 x 35793 x 4.0 GEO 70.3W
1978 Oct 18			1436.00 35780 x 35788 x 5.0 GEO 69.4W
1980 Feb 28			1436.12 35773 x 35800 x 5.9 GEO 69.8W
1982 Jul 12			1435.98 35774 x 35794 x 7.3 GEO 68.8W
1982 Nov 19		Drift	1436.16 35774 x 35800 x 7.6 GEO 69.7W+0.02
1983 Jan 11			1435.90 35775 x 35789 x 7.7 GEO 70.1W+0.04
1983 Feb 9		Move out	1435.45 35755 x 35792 x 7.7 GEO 61.3W+0.15W
1983 Mar 13		Move in	1435.76 35751 x 35808 x 7.8 GEO 53.1W
1983 Apr 27			1435.90 35741 x 35811 x 7.8 GEO 50.5W+0.04
1983 Aug?		Move out
1983 Sep 9			1435.54 35727 x 35823 x 8.0 GEO 77.5W+0.1W
1983 Nov 28			1435.98 35735 x 35833 x 8.2 GEO 71.4W+0.02

Kosmos 2090

 1990-070A

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Comsat D8-1 Replaced K1994/9

Kosmos-2090
Date	Time	Event	Orbit
1990 Aug 8	0415:07	Launch by Tsiklon-3	PL
		T+2:00 St 1 sep
		T+3:33 GO sep
		T+4:38 St 2 sep
		T+6:00 S5M burn 1 96s
	0422	T+7:36 S5M MECO-1	-200? x 1300 x 82.6
	0457?	T+41:50 S5M burn 2 22s
	0457?	T+42:10 S5M low thrust
	0457?	T+42:43 S5M sep first KA
		T+44:09 S5M sep last KA
1990 Aug 8			113.84 1390x1414x82.56

OSO 7

  1971-083A

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OSO H (Orbiting Solar Observatory 7) was launched at 0945 on 1971 Sep 29 by a two stage Delta N from Cape Canaveral. The Delta second stage had attitude control issues during the second burn, resulting in a low perigee orbit of 93.4 min, 323 x 571 km x 33.1 deg. The spacecraft observed the Sun until 1974 Jul 6 when its attitude control gas was depleted; it reentered on 1974 Jul 9 over the South Pacific.

OSO 7
Date	Time	Event	Orbit
1971 Sep 29	0945:00	Launch by Delta N	CC LC17A
		T+1:15 SRM 1-3 sep
		T+3:39 MECO
		T+3:42 St 1 sep
	0948:43	T+3:43 SES-1
	0948:50	T+3:50? Fairing
	0954:57	T+9:57 SECO-1
	1013:20	T+28:20 SES-2
	1013:27	T+28:27 SECO-2	93.4 323 x 571 x 33.1
	1018	T+33:15s S+0m St 2 sep
	1036	T+51:35s S+18m TETR sep from St 2
1973 May		end of MIT XR expt ops
1974 Jul 6		end of tx
1974 Jul 9		Reentered

Kosmos 1070

 1979-001A

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Two-tone telemetry?; Hi res satellite with 30KS capsule.

Kosmos-1070
Date	Time	Event	Orbit
1979 Jan 11	1500	Launch by Soyuz-U	Plesetsk
	1504	Blok-I burn
	1508	Blok-I sep
1979 Jan 11			89.52 206x297x62.81
1979 Jan 15			89.42 204x290x62.8
1979 Jan 19			89.34 201x284x62.8
1979 Jan 19		30KS separated
1979 Jan 20
	0714?	Deorbit
	0725?	PO sep
	0732?	Entry
	0748?	Landed

Aviation Week: July 8,1996

 https://welib.org/md5/2defbcf631efef08210c3c8c16f602a9