Kosmos 424

  1971-048A

---

Kosmos-424 was launched in May 1971 from Plesetsk and flew a 13 day mission.

Kosmos-424
Date	Time	Event	Orbit
1971 May 28	1030:00	Launch by 11A57	PL
	1034	Blok-I burn
	1038	Blok-I sep
1971 May 30	0657		89.35 198 x 286 x 65.4
1971 May 30	1430		89.36 204 x 282 x 65.40 (RAE)
1971 May 31	1411		89.34 195 x 287 x 65.4
		Orbit change
1971 Jun 1	1358		89.37 174 x 312 x 65.4
1971 Jun 7	2148		89.25 175 x 298 x 65.4
1971 Jun 9	1200?	Engine sep
1971 Jun 10	0316?	Retrofire
	0326?	PO sep
	0331?	Entry
	0347?	Landed after 12.71d

Apollo 13 (Odyssey)

  1970-029A

---

Apollo CSM 109 was assigned to Apollo 13, the third attempted landing mission, and named Odyssey. It was paired with LM 7 Aquarius.

At 0306 on Apr 14, the command to stir the cryo tanks was given; within a minute, an electrical fire had begun in Sector IV of the Service Module. At 0307:53 the fire caused Oxygen Tank No. 2 to explode; the side of the SM covering Sector IV was blown away and the CSM lost its electrical power, its oxygen supply, its water supply, and possibly its propulsion capability. The crew were 330000 km from Earth on a trajectory which threatened to strand them in space. The spaceship shook with a loud bang, and RCS jets fired to regain stability. Houston initially suspected erroneous readings, but as the crew saw their precious oxygen venting into space the seriousness of the situation became clear....

Odyssey (CSM 109)
Date	Time	Event	Orbit
1970 Apr 11	1913:00	Launch by Saturn V (SA-508)	KSC LC39A
	1915:15	S-IC CECO
	1915:44	S-IC OECO, S-IC sep
	1915:46	S-II ignition
	1916:14	Interstage sep
	1916:20	LES sep
	1918:31	S-II premature CECO
	1922:53	S-II OECO, sep
	1922:57	S-IVB ignition
	1925:30	S-IVB cutoff
	1925:40	Earth orbit insertion	88.32 184 x 198 x 32.6
	2148:46	S-IVB TLI burn
	2154:37	S-IVB cutoff
	2154:47	Translunar injection	217 x 566793 x 31.81
	2219:39	CSM sep from S-IVB/SLA	219 x 549183 x 31.74
		SLA panels sep
	2221	At 24m
	2230	CSM docked with LM
	2232	CSM hard docked
	2314:03	CSM/LM sep from S-IVB
1970 Apr 12	1215?	Pass h4 = EL1:4
1970 Apr 13	0153:50	MCC-2 burn, hybrid trajectory
	0153:53	MCC-2 CO	-146 x 553315 x 31.8
1970 Apr 14	0119	CDR and LMP to LM
	0300	CDR and LMP return to CM
	0306	SM cryo tank stir
	0307	Electrical fire in SM Sector IV
	0307:53	Explosion in Sector IV
	0451	LM transfer hatch open
	0551	CM power down, crew transfer to LM
	0906?	Equigravisphere
1970 Apr 17	1123	CM power up, crew transfer to CM
	1315	SM-109 jettison	41 x 836791 x 30.6
	1600	LM hatch closed
	1643:02	Undocked from LM	41 x 836196 x 30.6
	1753:47	Entry	43 x 947783 x 30.8
	1807:41	Splashdown 21 40S 165 22W Pacific
		Recovered by USS Iwo Jima

Soyuz 30 (Caucasus)

 1978-065A

---

Spacecraft 11F615A9 No. 67 was left over from the Almaz OPS 3 program. With no prospect for a near term Almaz 4 mission, it appears to have been converted for use as a DOS ferry. It was launched in June 1978 as Soyuz-30 and docked with the rear port of DOS 5 (Salyut-6) the following day. Soyuz-30 carried veteran Soviet astronaut Pyotr Klimuk and the first Polish astronaut, Miroslaw Hermaszewski.

Soyuz-30
Date	Time	Event	Orbit
1978 Jun 27	1527:21	Launch by Soyuz-U	KB
	1529	Blok BVGD sep
	1532	Blok A sep
	1536	Blok I MECO
	1536	Blok I sep
			88.8 194 x 244 x 51.6
1978 Jun 28	1300	TCM	264 x 310 x 51.6
	1708	Docked with DOS 5 +X port
	2010	Hatch open
1978 Jul 5	1015	Undocked
	1139	Landing program on
	1242?	Retrofire
	1245?	DO CO
	1300?	Modules sep
	1306?	Entry
	1330:20	Landed 300 km W of Tselinograd

Skynet 4A

 1990-001A

---

The Skynet 4 series were built by British Aerospace and Marconi, using the ECS bus.

Skynet 4A
Date	Time	Event	Orbit
1990 Jan 1	0007	Launch by Commercial Titan 3	CC LC40
	0008:49	Stage 1 ignition
	0009	SRM sep
	0011:27	Stage 2 ignition
	0011:38	Fairing sep
	0015:06	Stage 2 shutdown	165 x 612 x 28.6
	0118:52	Skynet 4A deployed
	0205?	PAM-D2 burn to GTO
	0207?	PAM-D2 burnout
	0210?	PAM-D2 sep
	0830?	Apo 1 over 58E
	1230?	Peri 1
	1900?	Apo 2 over 96W
	2230?	Peri 2
1990 Jan 2	0500?	Apo 3 over 110E
	0900?	Peri 3
	1500?	Apo 4 over 42W
	1900?	Peri 4
1990 Jan 3	0044?	AKM burn over 167E
	0130?	Apo 5 over 162E
1990 Jan 3			1380.42 33675 x 35703 x 3.4 GEO 170.1E+14.5E
1990 Jan 10			1382.67 33673 x 35794 x 3.4 GEO 80.8W+13.9E
1990 Jan 16			1419.99 35133 x 35808 x 3.4 GEO 42.1W+4.1E
1990 Jan 20			1428.19 35453 x 35809 x 3.4 GEO 27.1W+2.0E
1990 Jan 29			1427.54 35449 x 35788 x 3.4 GEO 7.8E+2.2E
1990 Feb 17			1436.12 35781 x 35793 x 3.4 GEO 6.0E
1990 Dec 10			1436.03 35652 x 35918 x 2.7 GEO 6.2E
1990 Dec 26		mv out
1991 Jan 11		mv in	1436.00 35731 x 35838 x 2.7 GEO 29.5E
1991 Mar 24			1436.03 35769 x 35800 x 2.6 GEO 29.5E
1991 Jun 20			1435.99 35732 x 35836 x 2.4 GEO 29.6E
1991 Jul 7			1436.03 35497 x 36073 x 2.5 GEO 29.2E
1991		Move to 65E?
1991 Oct 4			1435.71 35625 x 35932 x 2.8 GEO 65.4E+0.1E
1991 Oct 14			1435.73 35620 x 35738 x 3.0 GEO 65.6E
1991		Move to 34W
1992 Jan 3			1436.00 35771 x 35797 x 2.2 GEO 34.0W
1992 May 2			1436.12 35784 x 35789 x 2.0 GEO 34.0W
1994 Apr 30			1436.15 35774 x 35800 x 1.7 GEO 34.1W
1997 Oct 15			1436.12 35772 x 35801 x 3.0 GEO 34.0W
1999 Jun 16			1436.09 35782 x 35791 x 3.8 GEO 34.0W
2000 Sep 5			1436.11 35774 x 35798 x 5.6 GEO 34.5W

Kosmos 670

  1974-061A

---

The first of the new Soyuz class was 11F732 No. 1L, or 7K-S No. 1L. It was launched on an unpiloted test flight on 1974 Aug 6, into an unprecedented 50.6 degree inclination orbit, and recovered 3 days later. The craft was given the cover name Kosmos-670. The reentry was ballistic rather than lifting because of a problem at module separation. 

Kosmos-670
Date	Time	Event	Orbit
1974 Aug 6	0002:00	Launch by Soyuz	KB
	0004	Blok BVGD sep
	0006	Blok A sep
	0010	Blok I MECO
	0010	Blok I sep
1974 Aug 6			89.51 209x292x50.57
1974 Aug 7			89.51 209x292x50.57
1974 Aug 8			89.46 210x286x50.55
1974 Aug 9	0044?	DO 80m/s
	0048?	DO CO
	0100?	PAO sep
	0108?	Entry
	0130	Landed

Kosmos 1817

 1987-010A

---

The first Ekran-M satellite (11F647M No. 11L) was launched on 1987 Jan 30. It failed to reach its final orbit and was given the cover name Kosmos-1817. Kosmos-1817 was originally cataloged as 17367/1987-10C; sometime between 1993 and 1998 both the catalog number and (unusually) the archival TLEs associated with the catalog number were changed to 17365/1987-10A. Below the original designations are noted against the orbits.

Kosmos-1817
Date	Time	Event	Orbit
1987 Jan 30	0919	Launch by Proton	KB
	0928	Stage 3 sep
	1036?	Blok-DM failed to ignite
1987 Jan 30		(10A)	188x210x51.6
1987 Jan 30		(10B)	88.3 189x195x51.6
1987 Jan 30		(10C)	212x254x51.6 P/L
1987 Jan 30		(10D)	213x260x51.6
1987 Jan 31		(10A)	130x161x51.6, reentered Jan 31
1987 Feb 13		end of tx (AiK)
1987 Feb 21		(10C)	201x236x51.6
1987 Mar 15		(10C)	165x178x51.6
1987 Mar 17		(10C)	151x161x51.6
1987 Mar 18		(10C)	121x133x51.6
1987 Mar 18		(10C) reentered

Intelsat 4A2

  1976-010A

---

Intelsat 4A F2 was launched in Jan 1976 and became the AOR Primary Spare.

Intelsat IVA F-2
Date	Time	Event	Orbit
1976 Jan 29	2356	Launch by Atlas Centaur	CC LC36
	2358	Booster sep
1976 Jan 30	0000	Atlas sep
	0000:18?	MES-1
	0000:30?	Fairing
1976 Jan 30	0006:21?	T+10:21 Centaur MECO	184? x 1800? x 28.1?
	0020:30?	MES-2 2:05
	0022:35?	MECO-2
1976 Jan 30	0024	Centaur sep, Orbit insertion	578 x 36749
		Centaur venting
	0630?	Apo 1
	1700?	Apo 2
1976 Jan 31	0300?	Apo 3
	1400?	Apo 4
1976 Feb 1	0019	Apo 5, SVM-4A burn?
1976 Feb 1	0219	Apo 5, SVM-4A burn, over W POR
1976 Feb 2			GEO 140E +3E/d
			1420.2 35084 x 35869 x 0.11 (Fal)
1976 Feb		AOR Primary Spare	GEO 29.5W
1977 Jan 21			1436.15 35779 x 35796 x 0.0 GEO 29.6W+0.0
1978 May 25			1436.07 35781 x 35791 x 0.0 GEO 29.5W
1979 Jul 19			1436.11 35781 x 35792 x 0.0 GEO 29.5W+0.01W
1979 Jul 21		mv out	1435.82 35766 x 35785 x 0.1 GEO 28.9W+0.06E
1979 Aug 14		mv in	1436.15 35779 x 35796 x 0.0 GEO 27.4W+0.02W
1979 Sep		Domestic Lease, contingency	GEO 27.5W
1980 Jan 14			1436.13 35774 x 35799 x 0.0 GEO 27.5W+0.02W
1980 Oct 12			1436.10 35777 x 35795 x 0.0 GEO 27.4W+0.0W
1980 Oct 22			1436.13 35777 x 35796 x 0.0 GEO 27.5W+0.02W
1980 Nov?		Move to 21.5W
1980 Dec 2			1436.17 35778 x 35798 x 0.0 GEO 21.7W+0.03W
1981 Jan 2			1436.08 35776 x 35796 x 0.1 GEO 21.4W+0.0W
1981 Jun 11		AOR Major Path 2	GEO 21.5W
1981 Oct 2			1436.15 35778 x 35796 x 0.3 GEO 21.5W+0.02W
1982 Dec 18		Domestic lease/contingency	1436.13 35779 x 35794 x 0.0 GEO 21.5W
1983 Feb 21			1436.16 35783 x 35790 x 0.0 GEO 21.6W+0.01W
1983 Feb 21		mv out
1983 Mar 30			1436.16 35775 x 35800 x 0.2 GEO 56.9E+0.02W
1983 Apr		IOR domestic lease/contingency	GEO 57E
1983 Jun 1			1436.15 35774 x 35800 x 0.0 GEO 57.0E+0.02W
1984 Jan 11			1436.10 35783 x 35790 x 0.1 GEO 56.9E+0.0W
1984 Jan 17		mv out
1984 Mar 21			1438.08 35780 x 35870 x 0.3 GEO 46.8E+0.5W
1984 Aug 4			1437.25 35751 x 35867 x 0.6 GEO 2.8W+0.3W
1984 Aug		mv in, AOR Spare	GEO 4W
1984 Aug 17			1436.20 35749 x 35827 x 0.6 GEO 4.0W+0.03W
1984 Oct 1			1436.14 35750 x 35825 x 0.8 GEO 4.9W+0.02W
1985 Jan 13			1435.99 35759 x 35810 x 1.0 GEO 4.1W+0.02E
1985 Mar 15			1435.91 35755 x 35810 x 1.2 GEO 1.5W+0.04E
1985 Apr 13			1436.12 35761 x 35813 x 1.2 GEO 2.1W+0.01W
1985 Nov 27			1436.05 35759 x 35812 x 1.8 GEO 1.9E+0.0E
1985 Dec 19		orbit raise	1443.60 35910 x 35956 x 1.9
1987 Mar 1			1444.43 35925 x 35973 x 3.0
1990 Nov 25			1444.41 35930 x 35967 x 6.5
1995 Nov 24			1444.57 35924 x 35980 x 10.3
1999 Apr 28			1444.42 35941 x 35957 x 11.9

Brasilsat 1

 1985-015B

---

The SBTS 1 (Sistema Brasilero de Telecomunicacoes par Satelite) satellite was built by Spar and Hughes for Telebras (Telecomunicacoes Brasileiras), part of the Brazilian Ministry of Communications. Named Brasilsat 1 on reaching orbit, the HS376 satellite was operated by Embratel (Empresa Brasileira de Telecomunicacoes SA, Rio), the operational arm of Telebras.

In 1995 the satellite was leased by Hughes Communications Inc to provide supplemental C-band capacity for US domestic communications in the Galaxy system. In 2000 it was still in use by Panamsat; it was retired in 2002.

Brasilsat A1
Date	Time	Event	Orbit
1985 Feb 8	2322:00	Launch by Ariane 3	CSG
		T+0:30 PAP out
		T+0:33 PAP sep
		T+2:22 St 1 sep	-6100 x 100?
		T+2:22 Stage 2 burn
		T+3:37 Fairing sep
	2326:27	T+4:27 St 2 MECO
	2326:32	T+4:32 St 2 sep	-4700 x 225 x 9?
	2326:33	T+4:33 Stage 3 burn
	2338:40	T+16:40 Stage 3 MECO
	2341:12	T+19:12 Arabsat sep
	2342:12	T+20:12 SYLDA 4400 sep
	2343:45	T+21:45 Brasilsat 1 sep
1985 Feb 9
	0500?	Apo 1
	1030?	Peri 1
	1600?	Apo 2
1985 Feb 9	1534	Star 30B burn 20s
1985 Feb 9			1408.70 34666 x 35830 x 0.1 GEO 70.5W+7.0E
1985 Feb 11			1437.24 35778 x 35839 x 0.1 GEO 64.7W+0.3W
1985 Feb 11	0700?	Deploy antenna
1985 Feb 15			1436.04 35779 x 35791 x 0.1 GEO 64.8E+0.0E
1985 Apr 12			1436.10 35783 x 35789 x 0.0 GEO 65.0W+0.0W
1988 Jan 6			1436.17 35782 x 35793 x 0.0 GEO 65.2W+0.0W
1989 Dec 12			1436.17 35779 x 35796 x 0.0 GEO 65.0W+0.03W
1991 May 15			1436.16 35775 x 35800 x 0.1 GEO 65.0W+0.02W
1992 Oct 19			1436.12 35781 x 35793 x 0.1 GEO 65.0W+0.01W
1994 Apr 11			1436.16 35782 x 35793 x 0.0 GEO 65.1W+0.02W
1994 Nov 2			1436.11 35782 x 35791 x 0.1 GEO 64.9W
1994 Nov 7		mv out
1995 Jan 5		mv in	1436.11 35781 x 35792 x 0.3 GEO 63.2W+0.01W
1995 Jun 23			1436.17 35780 x 35795 x 0.6 GEO 62.8W+0.02W
1995 Oct		Leased by HCI
1996 Jun 2		1436.16 35782 x 35793 x 1.3 GEO 63.1W
1996 Jun 15		mv out	GEO 63W
1996 Jul 16		mv in	GEO 79.0W
1996 Sep 24			1436.13 35783 x 35790 x 1.6 GEO 79.0W
1997 May 16		Lease to Panamsat
1997 Jun 2			1436.15 35781 x 35793 x 2.1 GEO 79.1W
1998 Aug 29			1436.14 35778 x 35796 x 3.0 GEO 79.1W
1998 Aug 29		mv out	1439.04 35840 x 35847 x 3.0 GEO 92.2W+0.8W
1998 Dec 23		mv in	1436.11 35784 x 35788 x 3.1 GEO 144.0W
1999 Jun 10			1436.08 35777 x 35795 x 3.6 GEO 144.1W
2002 Mar 7			1436.04 35780 x 35791 x 5.6 GEO 144

Raduga 6

 1980-016A

---

Raduga No. 16 (Gran' 11F638 No. 16) was launched in Feb 1980 to the Statsionar 2 (35E) position. In Dec 1982 it was transferred to the Statsionar 9 (46E) position.

Raduga No. 16
Date	Time	Event	Orbit
1980 Feb 20	0805	Launch by Proton-K	KB
	0814	Stage 3 sep
	0922?	DM burn 1
	1438?	DM burn 2
	1442?	DM sep
			1464.95 36135 x 36563 x 0.6 GEO 89.8E+7.1W
1980 Feb 24			1474.50 36431 x 36638 x 0.6 GEO 48.7E+9.4W
1980 Feb 29			1441.23 35771 x 36002 x 0.4 GEO 35.3E+1.3W
1980 Mar 5		mv in	1436.37 35736 x 35847 x 0.3 GEO 35.2E
1980 Oct 2			1435.97 35749 x 35819 x 0.1 GEO 34.8E
1981 Oct 20			1436.11 35765 x 35808 x 0.9 GEO 34.2E
1982 Feb 12			1435.89 35754 x 35810 x 1.2 GEO 35.0E
1982 Feb 27			1435.92 35240 x 36325 x 1.2 GEO 36.4E+0.03E
1982 Mar 24			1436.20 35704 x 35872 x 1.3 GEO 34.4E+0.03W
1982 Apr 29			1435.93 35723 x 35843 x 1.3 GEO 34.7E+0.04E
1982 Sep 27			1436.16 35778 x 35797 x 1.7 GEO 34.0E
1982 Nov 28			1435.73 34843 x 36715 x 1.4 GEO 35.8E+0.09E
1982 Dec		mv to Statsionar 9
1982 Dec 4			1436.09 35720 x 35852 x 1.8 GEO 44.9E
1982 Dec 20			1435.73 35684 x 35874 x 1.9 GEO 46.1E
1983 Feb 23			1436.04 35712 x 35858 x 2.0 GEO 44.4E
1983 Nov 8			1436.16 35775 x 35800 x 2.6 GEO 44.2E
1983 Dec 29			1435.66 32604 x 38951 x 3.5 GEO 48.5E+0.1E
1984 Mar 6			1435.03 30435 x 41096 x 3.1 GEO 77.6E+0.26E
1984 May 31			1437.11 30499 x 41113 x 4.4 GEO 95.5E+0.3W
1984 Sep 9			1435.80 35760 x 35800 x 3.3 GEO 44.6E
1985 Mar 21			1435.92 35770 x 35796 x 3.9 GEO 44.9E
1985 Jun 28			1436.20 35786 x 35790 x 4.0 GEO 44.8E
1985 Oct 16			1435.95 35771 x 35796 x 4.4 GEO 44.7E
1985 Nov 7		last mv	1435.96 34939 x 3662 x 4.5 GEO 46.2E
1986 Jan 17			1435.86 35777 x 35786 x 4.6 GEO 45.0E
1986 Feb 5			1435.74 35775 x 35784 x 4.6 GEO 46.3E+0.08E
1986 Mar		end of ops
1986 Mar 13		Drifting	1435.52 35760 x 35789 x 4.8 GEO 50.6E+0.1E
1986 Nov 4			1435.56 35770 x 35781 x 5.3 GEO 99.8E+0.1E
1993 Jun 30			1435.49 35751 x 35797 x 11.0 GEO 98.4E+0.1E

Pioneer 7

  1966-075A

---

Pioneer B was launched at 1520:17 on 1966 Aug 17 by Delta E1 from Kennedy. The Delta separated at 1544:53 and the FW4 ignited at 1545:37. SP-278 and SP-280 give inconsistent values for the injection azimith corresponding to orbit inclinations of 22 and 42 deg respectively, with TR-1022 confirming the 42 deg value. Pioneer VII malfunctioned in 1972 Jul while at aphelion and lost some power, but it was still operable in 1980. 

Pioneer 7
Date	Time	Event	Orbit
1966 Aug 17	1520:17	Launch by Delta E1	CK LC17A
		T+0:42 SRM burnout
		T+1:11 SRM sep
	1522:45	T+2:28 Thor MECO 95 km	-5522 x 188
	1522	T+2:32 Delta burn 6:15
		T+2:33 Thor sep
		T+2:54 Fairing
	1529:04	T+8:47 Delta SECO
	1544:53	T+24:36 Delta sep	97.4 254 x 1022 x 33.00
	1545:37	FW4D burn, 30.8s
	1546:09	FW4D cutoff	367 x +Inf x 41.9
	1547:09?	FW4D sep
		Delta orbit	97.04 252 x 994 x 32.8
1966 Aug 26?		Solar orbit
1966 Sep 25		In geotail at 1000 Re
1966 Sep 26		XYZ(SE) = -900, 55, 22
1966 Sep 28		XYZ(SE) = -950, 85, 25
1966 Sep 30		XYZ(SE) = -1000, 130, 28
1972 Jul		Electrical system malfunction
1980		Still operational

Opera: May 2002

 https://welib.org/md5/7b2c7f61a064a8870bcb31f2c5e34453

Us Weekly: March 18,2002

 https://welib.org/md5/3264713601d97dbd38256728dae70b79

Molniya 319

 1982-083A

---

Molniya-3 (F21, N19) was launched in Aug 1982 into plane A. It originally failed to make any burns to stabilize its ground track, but in mid September it started a series of small burns and later that month it was on station to replace F15 (N13). It reportedly carried an experimental SHF transponder.

Molniya-3 No. 33
Date	Time	Event	Orbit
1982 Aug 27	0002	Launch by 8K78M	PL
		BVGD sep
		GO sep
		T+4:46 Blok A sep
		T+4:56 KhO sep
		T+8:46 Blok-I MECO
	0010	T+8:50 Blok-I sep
		T+53:16 BOZ burn
	0055	T+53:56 BOZ sep
		ML burn
		T+56:46 ML MECO
	0058	T+56:54 ML sep
1982 Aug 29			736.6 450 x 40827 x 62.9
1982 Sep 15		Begin TCM burns
1982 Nov 11			717.8 498 x 39856 x 62.9
1987 Apr 2		end of ops
2002 Jan 18		Reentered

My Perfect Guy

https://welib.org/md5/8279c94536461c5f68e7412337027c33

MARECS 2

 1984-114B

---

INMARSAT's second successful MARECS, leased from ESA, was launched in Nov 1984. The 1050 kg ECS-bus satellite was built by British Aerospace.

MARECS 2
Date	Time	Event	Orbit
1984 Nov 10	0114:18	Launch by Ariane 3 (V11)	CSG
		T+0:32 PAP sep
		T+2:15 St 1 MECO
		T+2:20 St 1 sep
		T+2:20 Stage 2 burn
		T+3:39 Fairing sep
		T+4:24 St 2 MECO
		T+4:29 St 2 sep
		T+4:32 Stage 3 burn
		T+4:43 St 3 ullage motors sep
	0130:50	T+16:32 St 3 MECO
		T+17:36 St 3 spinup
		T+17:51 St 3 spindown
	0132:41	T+18:23 Spacenet 2 sep from Sylda 4400
	0133:44	T+19:26 Sylda sep
	0135:21	T+21:03 MARECS 2 sep
1984 Nov 11	0324:33	Mage burn 43s
		Despin, uses 33 kg of hydrazine
		Solar array deploy
1984 Nov 11			1434.79 35606 x 35916 x 3.2 GEO 135.5E+0.3E
1984 Nov 13			1431.51 35600 x 35793 x 3.1 GEO 136.2E+1.1E
1984 Nov 16		Comms payload on
1984 Dec 9			1431.77 35634 x 35769 x 3.1 GEO 165.1E+1.1E
1984 Dec 19		Braking
1984 Dec 21		mv in	1436.33 35782 x 35800 x 3.0 GEO 177.5E
1985 Jan 8		Operational, POR Spare	GEO 177.5E
1986 Jan 14			1436.07 35773 x 35799 x 2.4 GEO 177.5E
1986 Jan 15		Traffic to MCS-D
1986 Jan 15		mv out	GEO 177.5E dr
1986 Feb 15			1456.60 36178 x 36195 x 2.3 GEO 17.8E+5.1W
1986 Feb 25		AOR Primary, replaced MARECS 1	GEO 26W
1986 Mar 2			1436.08 35769 x 35802 x 2.3 GEO 25.9W
1987 Sep 25			1436.11 35774 x 35799 x 1.9 GEO 26.0W
1989 Sep 7			1436.04 35772 x 35798 x 3.0 GEO 26.0W
1990 Aug 31			1436.11 35775 x 35798 x 3.2 GEO 26.1W
1990 Sep 19			1436.15 35773 x 35802 x 2.2 GEO 25.9W+0.02W
1990 Nov		Moved to make new region
1990 Nov 11			1436.16 35776 x 35799 x 1.7 GEO 55.4W+0.02W
1990 Nov 19			1436.09 35774 x 35798 x 1.7 GEO 55.3W
1992 Jun 26			1436.08 35774 x 35798 x 3.1 GEO 55.4W
1992 Jul 7		mv out	1432.16 35689 x 35729 x 3.1 GEO 43.6W+0.9E
1992 Aug 11		mv in
1992 Sep 2			1436.07 35774 x 35798 x 3.2 GEO 15.1W
1993 Mar 21			1436.09 35765 x 35807 x 3.7 GEO 15.0W
1996 Mar 15			1436.10 35770 x 35803 x 6.0 GEO 15.0W
1997 Jan 30			1436.13 35764 x 35810 x 6.6 GEO 15.5W
1997 Feb		Move to 26W
1997 Feb 20			1436.05 35771 x 35800 x 6.7 GEO 25.9W
1999 May 17			1436.15 35769 x 35805 x 8.1 GEO 26.1W
2002 Jan 18			1436.11 35769 x 35803 x 9.60 GEO 26.3W

Club Management: April 2002

 https://welib.org/md5/dba9a2c95fa1f47f5a8660133ed6c36a

February 10,2000

 https://planet4589.org/space/jsr/back/news.420.txt

Raduga 32

 1994-087A

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Raduga (Gran' 11F638) No. 43, Raduga (F33, N32), was launched on 1994 Dec 28. It operated until late 2000 or early 2001.

Raduga 43L
Date	Time	Event	Orbit
1994 Dec 28	1131	Launch by Proton-K	KB LC81
	1140	Stage 3 sep
	1240?	DM burn 1
	1750?	DM burn 2
	1810?	DM sep
			1438.13 35740 x 35912 x 2.0 GEO 90.1E
1995 Jan 1			1439.23 35787 x 35906 x 1.5 GEO 87.1E+0.8W
1995 Jan 16			1436.24 35784 x 35794 x 1.4 GEO 70.6E
1995 Mar 5			1436.21 35784 x 35792 x 1.4 GEO 69.0E
1996 May 11			1435.99 35777 x 35791 x 0.5 GEO 71.0E
1999 Oct 17			1436.07 35777 x 35794 x 2.1 GEO 70.1E
2000 Nov 24			1436.00 35777 x 35791 x 3.0 GEO 70.9E

Koronas-I

 1994-014A

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A new generation of AUOS satellites, the AUOS-SM, was introduced by Koronas-I, the first science satellite launched by the Russian Space Agency. KORONAS is an acronym for Kompleksnie Orbital'nie Okolozemnie Nablyudeniya Aktivnosti Solntsa (Near Earth Orbital Complex for Studying Solar Activity). The I stands for IZMIRAN (Institut Zemnovo Magnetizma, Ionosferi i rasprostraneniya radiovoln AN Rossii), the terrestrial magnetism and ionospheric research institute of the Russian Academy Of Sciences. Koronas had the prelaunch designation AUOS-SM-KI-IK ( AUOS-SM-KI-IK) No. 801. The satellite was a 2298 kg 3-axis stabilized cylinder with solar panels. It was 5.0 m high and 2.3m in diameter, with a span of 12.8m once deployed. The satellite achived 40 arcsecond pointing (only 10 arcmin was required).

Koronas-I
Date	Time	Event	Orbit
1994 Mar 2	0325	Launch by 11K68 Tsiklon-3	NIIP-53 LC32
	0327:00	T+2:00 Stage 1 sep (alt 48.1km)
	0329:37	T+4:37 Stage 2 sep (alt 147.5 km)
	0330:20	T+5:20 S5M burn 1 (alt 170.7 km)
	0332:04	S5M MECO1 (alt 193.1 km, in transfer orbit)	170? x 507 x 82.5
	0415:00	S5M burn 2 (alt 506.4 km)
	0415:09	S5M MECO2 (alt 507.1 km)
	0415:39	S5M sep	94.78 488 x 528 x 82.5
1994 Jul?		lost attitude control
1995 Apr		end of ops?
2001 Mar		Reentered

Payload:

• Terek Soft XR telescope-coronagraph spectroheliometer