Approaches to Teaching the Arthurian Tradition

https://welib.org/md5/e8b4b171c8f1b640436dcaf59f9f77b2

Progress M-2

 1989-099A

---

7K-TGM No. 202 (Progress M-2) was launched on 1989 Dec 20. 

Progress M-2
Date	Time	Event	Orbit
1989 Dec 20	0330:50	Launch by Soyuz-U	KB
			88.48 187 x 211 x 51.6
	0930		91.16 271 x 391 x 51.6
1989 Dec 22			91.18 275 x 390 x 51.6
	0500		92.42 392 x 394 x 51.6
	0541:21	Docked with Mir, Kvant DP2
1989 Dec 25	1900		92.41 391 x 393 x 51.6
1990 Feb 8	2130		92.46 381 x 408 x 51.6
1990 Feb 9	0233	Undocked frm Kvant DP2
	0500	Relay tests with Kosmos-2054
	0710	Deorbit
	0756	Reentered

Kosmos 2007

 1989-024A

---

Kosmos-2007
Date	Time	Event	Orbit
1989 Mar 23	1225:00	Launch by Soyuz	Plesetsk
	1234	Blok-I sep
1989 Mar 23			89.10 182x278x64.8
1989 Mar 24			89.64 229x283x64.8 from 89.02 181x271x64.8
1989 Mar 24			89.66 230x285x64.8
1989 Mar 31			89.79 219x309x64.7 from 89.36 219x266
1989 Apr 5			89.51 233x268x64.7 from 89.19 211x258
1989 Apr 6			89.83 238x295x64.7 from 89.46 230x265
1989 Apr 17			89.62 218x293x64.7 from 89.28 219x259
1989 Apr 19			89.87 236x300x64.7 from 89.53 216x287
1989 May 2			89.80 238x291x64.7 from 89.41 222x269
1989 May 12			89.79 235x294x64.7 from 89.40 225x264
1989 May 22			89.78 224x304x64.7 from 89.40 220x262
1989 May 30			89.88 243x295x64.7 from 89.48 216x282
1989 Jun 15			89.79 236x291x64.7 from 89.32 222x259
1989 Jun 25			89.61 226x283x64.7 from 89.36 222x263
1989 Jun 26			89.72 236x284x64.7 from 89.61 226x283
1989 Jul 3			89.65 227x287x64.7 from 89.37 224x261
1989 Jul 4			89.73 235x287x64.7 from 89.65 227x287
1989 Jul 15			89.47 233x263x64.7 from 89.37 223x263
1989 Jul 16			89.74 232x291x64.7 from 89.43 231x260
1989 Jul 27			89.78 236x290x64.7 from 89.34 219x264
1989 Aug 11			89.60 217x292x64.7 from 89.22 215x256
1989 Aug 12			89.76 235x290x64.7 from 89.56 215x289
1989 Aug 23			89.67 217x296x64.7 from 89.31 219x261
1989 Aug 24.6			89.62 216x294x64.7
1989 Sep 7			89.27 218 x 257 x 64.7
1989 Sep 8		Orbit raise	89.64 217 x 295 x 64.7
1989 Sep 9		Orbit raise	89.82 235 x 295 x 64.7
1989 Sep 21			89.18 213 x 254 x 64.7
1989 Sep 22		reentered

Kosmos 1814

 1987-006A

---

Kosmos-1814
Date	Time	Event	Orbit
1987 Jan 21	0910:00	Launch by 11K65M	Plesetsk 41.52E
		Stage 2 burn
	0918?	T+8 min Stage 2 MECO-1
		Stage 2 MES-2
	0944?	T+34min Stage 2 MECO-2
		Stage 2 sep
1987 Jan 25			771x810x74.06

Kosmos 1445

 1983-017A

---

The second BOR-4 orbital test made 1.5 orbits and landed in the Indian Ocean 550 km south of the Cocos Islands.

BOR-4 flight 2
Date	Time	Event	Orbit
1983 Mar 15	2230	Launch by K65MP	GTsP4
	2232?	Stage 2 burn
	2238?	Stage 2 sep
1983 Mar 16			88.51 177 x 224 x 50.69
1983 Mar 16			88.41 173 x 218 x 50.7
	0008?	Deorbit	-211? x 223 x 50.7
	0026?	Entry
	0041?	Landing

Kuafu 1

 1994-010B

---

The first test flight of the uprated CZ-3A launch vehicle carried a model of the DFH-3 satellite. It was named KF 1 (Kua Fu), after a mythical character. Mass was 1342 kg. Shape was 2.5 dia 2.2l cylinder + cone.

DFH-3 Mockup
Date	Time	Event	Orbit
1994 Feb 8	0830	Launch by CZ-3A	XSC
		T+2:25 Stage 1 MECO
		T+2:27 Stage 2 MES, Stage 1 sep 57 km	-6000 x 90?
		T+3:52 Fairing 119 km	-5440 x 150 ?
		T+4:15 St 2 MECO 134 km
		T+4:20 St 2 VECO 138 km
		T+4:21 St 2 sep, St 3 MES 138 km	-5130 x 170?
	0840	T+10:19? St 3 MECO-1 195 km
	0850	T+20:00? St 3 MES-2
	0852	T+22:00? St 3 MECO-2
	0853	T+23:40? Stage 3 sep	637.09 208 x 36086 x 28.6
1999 Sep 4			322.70 158 x 18254 x 28.4

Gambit-3 15

  1968-064A

---

KH-8 15 was launched on 1968 Aug 6 by Titan 3B Agena D from Vandenberg. The spacecraft reentered after only 9 days and it has been suggested that it performed poorly, but the short lifetime is not inconsistent with other missions around this time and the Perry history reports a nominal flight with good resolution imagery.

KH-8 15
Date	Time	Event	Orbit
1968 Aug 6	1630	Launch by Titan IIIB Agena D	V SLC4W
	1632	Titan stage 1 sep
	1632	Titan stage 2 sep
	1635	Agena burn
	1640	Agena MECO
1968 Aug 6	2331		90.13 120 x 441 x 110.0
1968 Aug 11	0057		89.63 118 x 393 x 110.0
		Orbit adjust
1968 Aug 14	0104		90.14 109 x 452 x 110.0
		Orbit adjust
1968 Aug 14	1723		90.07 118 x 436 x 110.0
1968 Aug 16
	2055?	SRV-1 sep
	2102?	Entry
	2130?	SRV-1 recovered
	2235?	Deboost rev 163

The saddle club collection : Hoof beat : Riding camp : Horse wise

 https://welib.org/md5/d3312037e581a1f581469bcb0f1b30be

Kosmos 1571

 1984-058A

---

The TsSKB web site gives this launch as the first Zenit-8 launch. The VKS history talks about Zenit-8 test flights in 1979-83, but I think it's in error (confusion between Zenit-4MKM, Zenit-6 and Zenit-8?).

Kosmos-1571
Date	Time	Event	Orbit
1984 Jun 11	0840	Launch by Soyuz	KB
	0844	Blok I burn
	0848	Blok I MECO
	0848	Blok I sep
			210 x 376 x 70
1984 Jun 12			349 x 413 x 70
1984 Jun 26	0330?	KDU sep
	0430?	Deorbit burn over 58S
	0441?	PO sep	-73 x 390 x 70.0
	0500?	Reentry
	0511?	Landed

Galaxy 3

 1984-101A

---

Hughes Communications Inc.'s third HS376C Galaxy went up a year after the second. It was used mostly for cable TV distribution and, initially, as an in-orbit spare.

Galaxy III
Date	Time	Event	Orbit
1984 Sep 21	2218	Launch by Delta 3920	CC LC17
		T+0:57 SRM 1-5 off
		T+1:02 SRM 1-3 sep
		T+1:02 SRM 6-9 on
		T+1:05 SRM 4-5 sep
		T+2:01 SRM 6-9 off
		T+2:06 SRM 6-9 sep
		T+3:44 MECO
		T+3:52 St 1 sep
		T+3:57 SES-1
	2222	T+4m Fairing
	2229	T+11:05 SECO-1	170 x 270? x 28.5
	2238	T+20:14 St 2 sep
	2238	T+20:52 Star 48 burn 86s
	2240	T+22:18 Star 48 burnout
	2242	T+24:26 Star 48 sep	654.49 199 x 36985 x 23.15
	2250	St 2 depletion	91.07 271 x 382 x 27.1
1984 Sep 22			664.19 697 x 36979 x 21.3
	0400?	Apo 1 over 90E
	1500?	Apo 2 over 74W
1984 Sep 22	1511?	Star 30 burn 9th apo 54s
1984 Sep 22			1452.58 35260 x 36956 x 0.3 GEO 77.7W+4.1W
1984 Sep 24			1449.49 35749 x 36346 x 0.2 GEO 80.2W+3.3W
1984 Oct 1			1436.24 35775 x 35803 x 0.2 GEO 93.5W
1986 Dec 1			1436.04 35780 x 35790 x 0.0 GEO 93.4W
1988 Mar 20			1436.15 35780 x 35795 x 0.0 GEO 93.6W
1990 Mar 19			1436.10 35777 x 35795 x 0.0 GEO 93.5W
1992 Apr 19			1436.12 35773 x 35800 x 0.0 GEO 93.6W
1994 Jun 15			1436.12 35778 x 35795 x 0.0 GEO 93.6W

Soyuz T-12 (Pamir)

 1984-073A

---

Soyuz T-12 (7K-ST 11F732 No. 18L) was launched in Jul 1984.

---

Crew

---

• Komandir Pol. Vladimir Dzhanibekov, VVS

• Bortinzhener Svetlana Savitskaya, NPO Energiya

• Kosmonavt-issledovatel' Igor Volk, Min. Av.

Soyuz T-12, Flight 1
Date	Time	Event	Orbit
1984 Jul 17	1741	Launch by Soyuz-U	KB
	1743	Blok-BVGD sep
	1745	Blok-A sep
	1749	Blok-I cutoff
	1749	Blok I sep
			198 x 224 x 51.6
			226 x 308 x 51.6
			334 x 354 x 51.6
1984 Jul 18	1917	Docked +X

Soyuz T-12, Flight 2
Date	Time	Event	Orbit
1984 Jul 29	0926	Undocked
	1139	BO sep
	1202?	DO
	1206?	DO CO
	1228?	PAO sep
	1233?	Entry
	1256:30	Landed

DAPP 9

 1964-031A

---

The second pair of twins was launched five months after the first. Both satellites were deployed successfully. The AFCRL list quotes a cosmic ray emulsion pack as being recovered from "18 Jun 64 1964-31A", but this is almost certainly an error and should refer to the next day's CORONA flight "19 Jun 64 1964-32A". The Vandenberg launch report includes no reference to a capsule recovery and NRO documents confirm a dual metsat payload was carried. The Vandenberg launch report quotes an actual inclination of 100.6 deg, while subsequent orbital data shows the true value to be 99.8 deg, much closer to the planned value - the 100.6 figure is probably a typo.

OPS 4467A
Date	Time	Event	Orbit
1964 Jun 18	0456:08	Launch by Thor Agena D	V
	0458:34	Thor MECO (T+2:26)
	0458:43	Thor VECO (T+2:35)
	0458:48	Thor sep (T+2:40)
	0459:31	Agena burn (T+3:23)
	0503:30	Agena MECO (T+7:22)	-470? x 830 x 99.8
	0550:00	Agena burn 2 (T+53:52) 4.0s
	0550:04	Agena MECO (T+53:56)	101.6 836 x 846 x 100.6 (VCR)
		Payload 4467A ejected from Agena 2304
		Payload 4467B ejected from Agena 2304
1964 Jun 18	0930		101.64 828 x 842 x 99.8 (RAE)
1966 Feb 16		End of ops

STS-61-A (Challenger)

 1985-104A

---

Challenger's third Spacelab mission in a row was Spacelab D-1, the first German Spacelab flight. Launch was on 1985 Oct 30.

STS 61-A
Date	Time	Event	Orbit
1985 Oct 12			VAB 1
1985 Oct 16		Rollout	LC39A
1985 Oct 30	1700:00	Launch	LC39A
	1702:05	SRB sep, 49.4 km
	1708:35	MECO, 113.6 km
	1708:54	ET sep, 115.6 km	86.76 45? x 182? x 57.0
	1710:35	OMS 1 (2:01) 59.6m/s	88.77 97 x 330 x 57.0
	1712:37	OMS 1 CO
	1744:40	OMS 2 (2:13) 67.5m/s	91.07 321 x 332 x 57.0
	1746:56	OMS 2 CO
	1825	PLBD open
	2000?	SL-D1 activation
1985 Oct 31	0534	GLOMR deploy	91.07 321 x 332 x 57.0
			322 x 333 x 57.0
1985 Nov 6	1326	PLBD closed	91.06 321 x 331 x 57.0
	1640:30	OMS DO (170s) 91.9m/s
	1643:21	OMS DO CO
	1713:32	Entry
	1744:51	Landing	RW17 EAFB
	1744:59	NGTD
	1745:40	Wheels stop
1985 Nov 10	1600	SCA 905	EAFB
	2145	SCA 905	Davis-Monthan AFB, AZ
1985 Nov 11	1725	SCA 905	Tyndall AFB, FL
	1835	SCA 905	KSC SLF
	2305		OPF/1

Tiros-N

 1978-096A

---

Tiros N, the prototype for the Tiros N series, was launched on 1978 Oct 13 by Atlas F from Vandenberg into a suborbital trajectory on azimuth 192.8 deg. The Star 37S (TE-364-15) solid motor fired at apogee, inserting the payload into a 850 x 866 km x 98.9 deg, 102.1 min orbit with 0300LTDN afternoon orbit. After several weeks of system checkout, NASA transferred the satellite to NOAA-NESS and it entered operational service on 1979 Jan 1. On 1981 Feb 27 Tiros N lost attitude control and was abandoned.

Tiros N was 3.71m high 1.88m dia with a launch mass of 1405 kg. At BOL, mass is 723 kg after AKM and RCS burns. AKM is 48 kg with 664 kg of prop:

Tiros N dry	675
AKM dry	48
Tiros N BOL	723
AKM prop	664
RCS prop	18
Full	1405 kg

Tiros N
Date	Time	Event	Orbit
1978 Oct 13	1123	Launch by Atlas F	V SLC3W
		T+2:01 BECO
		T+2:04 Booster sep
		T+2:24 Fairing sep
		T+5:24 SECO
		T+5:43 VECO
	1128	T+5:49 Atlas sep, 896 km
	1133	T+10:27 AKM burn 43s
	1134	T+11:10 AKM burnout
	1134	T+11:15 RCS trim
	1134	T+11:38 RCS cutoff	102.07 848 x 863 x 98.91
		T+13:47 Solar array deploy
		Atlas impact, 7770 km range
1994 May 21			101.59 825 x 842 x 98.93

Payload:

• AVHRR Advanced Very High Resolution Radiometer, 1 km res operating at 0.55-0.90, 0.725-1.10, 3.55-3.93, 10.5-11.5 and 11.5-12.5 mu, for cloud mapping, water imaging, and sea surface temperature.

• TOVS Tiros-N operational vertical sounder

  • SSU Stratospheric sounding unit 147 km res, CO2 15 mu band

  • MSU Microwave sounding unit 109 km res, O2 50-57 GHz band

  • HIRS/2 Tropospheric Hi res IR radiation sounder 17 km res, 0.7 mu vis and 3.7, 4.3, 6.7, 9.7, 11, 15 mu IR (CO2, O3, H2O)

• DCS/ARGOS Data collection system (CNES), 401 MHz

• SEM Space Environment Monitor (measures solar X-rays and particle fluxes)

  • TED Total energy detector, 0.3-20 keV

  • MEPED Med energy p/e, 30 - 60 keV

  • HEPAD High energe p/alpha, 0.37-850 MeV

Resurs 38

 1991-058A

---

The 13th named Resurs F flight was Resurs F-2 No. 7, carrying the MK-4 multispectral camera payload. It again used the new, lower Resurs F-2 orbit.

Resurs F-2 No. 7
Date	Time	Event	Orbit
1991 Aug 21	1050	Launch by Soyuz	PL LC43/3
	1054	Blok-I burn
	1058	Blok-I sep
1991 Aug 29			89.07 224 x 232 x 82.31
1991 Sep 4			89.09 222 x 236 x 82.3
1991 Sep 5			89.13 229 x 234 x 82.3
1991 Sep 7			89.08 226 x 232 x 82.3
1991 Sep 8			89.15 231 x 233 x 82.3
1991 Sep 11			89.05 226 x 228 x 82.3
1991 Sep 12			89.16 226 x 239 x 82.3
1991 Sep 15			89.06 221 x 234 x 82.3
1991 Sep 16	1633		89.14 231 x 232 x 82.3
1991 Sep 20	0057		89.04 226 x 228 x 82.3
1991 Sep 22
	0518?	Deorbit
	0528?	PO sep
	0535?	Entry	-204 x 227
	0550?	Landed

Progress M-6

 1991-002A

---

11F615A55 (7K-TGM) No. 205 became Progress M-6 when launched in Jan 1991.

Progress M-6
Date	Time	Event	Orbit
1991 Jan 14	1450:27	Launch by Soyuz-U	KB
	1600		88.42 187 x 204 x 51.6
	2130		90.42 248 x 342 x 51.6
1991 Jan 16	1635:25	Docked with Mir/KDP2
1991 Jan 21			92.15 362 x 397 x 51.6
1991 Mar 14	0500		92.14 368 x 391 x 51.6
1991 Mar 15	1246:41	Undocked
	1340		91.78 336 x 387 x 51.6
	1702		91.78 336 x 387 x 51.6
	1714	Deorbited
	1807:26	Reentered

USA-45

 1989-072A

---

A Russian report claimed that the second Titan 23G test satellite, USA-45, reentered after 7 days from the initial parking orbit because of the failure of its motor.

USA 45
Date	Time	Event	Orbit
1989 Sep 6	0148?	Launch by Titan 23G	V SLC4W
		T+2:30? Stage 1 sep
		T+2:30? Stage 2 burn
		T+3:45? Fairing
		T+5:25? Stage 2 MECO
	0153	T+5:30? Stage 2 sep	185 x 300 x 85? (Speculation)
1989 Sep 13?		Reentered

Variety: August 8-14,1994

 https://welib.org/md5/639ea8bd26f95995d5c0cf647a9ee130

Kosmos 279

 1969-038A

---

Zenit-4 No. 61 was launched into a 51.7 degree orbit from Baikonur in Apr 1969. According to Charles Sheldon's congressional reports it carried an ion orientation system test.

Kosmos-279
Date	Time	Event	Orbit
1969 Apr 15	0814:59	Launch by 11A57	KB
	0819	Blok-I burn
	0824	Blok-I sep
	2255		89.18 193 x 274 x 51.7
1969 Apr 18	0238?	Blok-I reentered
	0930		89.04 192 x 267 x 51.74
1969 Apr 21			88.99 189 x 258 x 51.7
1969 Apr 23	0730?	Retrofire
	0750? Landed

Journal of the British Interplanetary Society: July 1994

 https://welib.org/md5/03c75928d581787527863f31ff0b1dd6

Kosmos 2107

 1990-108A

---

RCS was 20m2.

Kosmos-2107
Date	Time	Event	Orbit
1990 Dec 4	0048:31	Launch by 11K69	Baikonur
	0050	Stage 1 sep
	0052	Stage 2 sep
	0136?	AKM burn
1990 Dec 5			92.78 404x417x65.0
1992 Jan 23			92.78 403x418x65.0
1992 Mar 9			92.78 403x418x65.0
1992 Mar 11			90.86 226x407x65.0
1992 Mar 19			90.40 215x372x65.0
1992 Mar 26			89.90 204x334x65.0
1992 Apr 2			89.10 182x277x65.0
1992 Apr 5		reentered

Sunset Passion

 https://welib.org/md5/0072352509e9863097032ea9be6a2856

Meteor 209

 1982-116A

---

Meteor-2 (F9) was launched in Dec 1982, returning to use of the Vostok rocket.

Meteor-2 (F9)
Date	Time	Event	Orbit
1982 Dec 14	2230	Launch by Vostok 8A92M	PL
	2234?	Blok E burn
	2240?	Blok E MECO
		Blok-E sep	102.0 812 x 892 x 81.3
1985?		End of ops

Publishers Weekly: July 4,1994

 https://welib.org/md5/eda525092bc3fc80e5d9346dcfd59894

Kosmos 2138

 1991-023A

---

Kosmos-2138
Date	Time	Event	Orbit
1991 Mar 26	1345:00	Launch by Soyuz	PL
	1353	Blok-I sep
1991 Mar 26.68			89.59 163x345x67.14
1991 Mar 30.1			90.07 192x363x67.15 from 89.19 158x310
1991 Apr 3.2			89.84 186x347x67.14 from 89.33 157x325
1991 Apr 14.9			89.16 167x299x67.1 from 88.90 165x274
1991 Apr 15		SpK-1 fid
1991 Apr 18.7			89.76 161x363x67.1 from 89.03 162x290
1991 Apr 23.2			89.62 188x322x67.1 from 89.17 155x311
1991 Apr 29.2			89.77 187x339x67.1 from 89.16 179x286
1991 May 4		SpK-2 fid
1991 May 6.9			89.73 182x339x67.1 from 89.18 176x290
1991 May 18.1			88.51 161x240x67.1 from 88.43 159x234
1991 May 18.8			89.78 186x340x67.1 from 88.44 167x226
1991 May 22.6			89.54 183x320x67.1
1991 May 24
	1753?	Deorbit
	1807?	Entry
	1820?	Landed

Myojo

 1994-007B

---

The first test launch of the H-II heavy launch vehicle carried a Vehicle Evaluation Payload (VEP). The 2400 kg VEP was the ETS-6 ground test model, and consisted of vehicle monitoring instruments, attached to the first LAPS liquid apogee stage. The LAPS stage carried 1470 kg of propellant ballast. VEP was named Myojo (Morning/Evening Star) once in orbit. VEP took off aboard H-2-1F from the Yoshinobu complex at Tanegashima on 1994 Feb 3.

Myojo
Date	Time	Event	Orbit
1994 Feb 3	2220	Launch by H-II (H-2-1F)	TNSC
	2221	SRB sep (T+1:39) 40 km 1.6 km/s
	2223	Fairing sep (T+3:40) 130 km 2.8 km/s
	2226	LE-7 MECO, (T+5:56) 227 km 5 km/s?	-4600 x 300 ?
	2226	T+6:06 Stage 1 sep
	2226	LE-5A SEIG1 (T+6:12)
	2233	LE-5A SECO1 (T+12:55), 454 km
	2234	OREX sep (T+13:50)	454 x 454 x
	2245	LE-5A TIG2 (T+24:56), 2:46
	2247	LE-5A MECO2 (T+27:36)
	2248	VEP sep (T+27:56), 467 km
1994 Feb 6	1200		642.00 468 x 36078 x 28.54

Fortune: August 22,1994

 https://welib.org/md5/84fde43807847bdf5342328a10e0bd67

Kosmos 1663

 1985-052A

---

Resurs F-1 17F41 No. 55 (Kosmos-1663) flew a 15 day mission in Jun-Jul 1985.

Kosmos-1663
Date	Time	Event	Orbit
1985 Jun 21	0745	Launch by Soyuz-U	PL LC41
	0753	Blok-I sep	216 x 270 x 82.3
1985 Jun 22			260 x 274 x 82.3
1985 Jul 1			262 x 278 x 82.3
1985 Jul 5			262 x 277 x 82.3
1985 Jul 6
	0402?	Deorbit
	0410?	PO sep
	0422?	Entry
	0437?	Landed

Kosmos 332

  1970-028A

---

Kosmos-332 entered the standard 100 minute period Tsiklon orbit in Apr 1970.

Kosmos-332
Date	Time	Event	Orbit
1970 Apr 11	1700:00	Launch by 11K65M	PL
	1702?	Stage 2 burn
	1708?	Stage 2 coast
	1755?	Stage 2 burn 2
	1755?	Stage 2 sep
1970 Apr 12	0930		100.01 755 x 761 x 74.05

Kosmos 1287

 1981-074A

---

Kosmos-1287 was satellite 1 of Strela-1M octuplet no. 28.

Kosmos-1287
Date	Time	Event	Orbit
1981 Aug 6	1149	Launch by 11K65M	PL
		Stage 2 burn 1
	1156	T+7m Stage 2 MECO-1
		Stage 2 burn 2
	1247?	T+58m? Stage 2 sep
			115.79 1466 x 1515 x 74.03

Zond 6

  1968-101A

---

The L-1 No. 12 spacecraft was launched on the Zond-6 mission. A faulty gasket around the hatch caused partial depressurization of the descent module, and as a further result the parachute system malfunctioned during descent and the spacecraft impacted the Earth's surface only 18 km from the launch site.

Zond-6
Date	Time	Event	Orbit
1968 Nov 10	1911	Launch by Proton-K	KB
	1920	Stage 3 sep
	1921	Blok D burn 1
	1923?	Blok D MECO-1
	2010?	SOK cone sep	165 x 199 x 51.5
	2018:30	Blok-D burn, TLI
	2018	SOZ units sep
	2025?	Blok-D MECO-2
	2026?	Blok D sep
1968 Nov 12	0540:39	TCM 8.5s at 246000 km
1968 Nov 14	0249	LOS
1968 Nov 14	0300?	Perilune 2420 km
	0321	AOS
1968 Nov 16	0640	TCM at 236000 km	25 x 400000?
	1025	SA depressurized to 380 mm due to faulty gasket
1968 Nov 17	0536	TCM 3s at 120000 km	45 x 400000?
	1345	PAO sep
	1352	Entry 1, skip out of atmosphere	100? x -800? x ?
	1354	Spacecraft depress to 25mm
	1358	Entry 2 in USSR
	1409	Parachute jettison early at 5 km
	1412	Impact, damaged but photos recovered