Soyuz 29

 1978-061A

---

7K-T 11F615A8 No. 46 was launched on 1978 Jun 15 with the DOS-5 EO-2 crew, Vladimir Kovalyonok and Aleksandr Ivanchenkov. It was named Soyuz-29. Soyuz-29 docked with the front port on Salyut-6 on Jun 16.

On Sep 3, the EP-4 Interkosmos crew of Valeriy Bykovskiy and Sigmund Jahn entered the spacecraft and undocked, returning to Earth later that day.

Soyuz-29
Date	Time	Event	Orbit
1978 Jun 15	2016:45	Launch by Soyuz-U	KB
	2019	Blok BVGD sep
	2021	Blok A sep
	2025	Blok I MECO
	2026	Blok I sep
			88.8 193 x 248 x 51.6
			253 x 309 x 51.6
1978 Jun 16			338 x 353 x 51.6
	2158	Docked
1978 Sep 2	1400	Test burn
1978 Sep 3	0645	Crew entry
	0823:18	Undocked
	1052:09	Retro
	1055?	DO CO
	1110:32	PAO, BO sep
	1116?	Entry
	1140:34	Landed 140 km SE of Dzezkazgan

FSW-21

 2005-027A

---

FSW launched in Aug 2005.

FSW
Date	Time	Event	Orbit
2005 Aug 2	0730:03	Launch by CZ-2C	JQ
	0740?	Stage 2 MECO
	0750		91.12 165 x 493 x 63.0
2005 Aug 3	0400	Orbit tweak	91.14 166 x 494 x 63.0
2005 Aug 4	2025		91.10 166 x 491 x 63.00
2005 Aug 5		Orbit raise
	1915		91.49 166 x 528 x 63.0
2005 Aug 7		orbit raise
	0603		91.73 166 x 552 x 63.0
2005 Aug 10	1952		91.65 166 x 544 x 63.0
2005 Aug 18			91.56 167 x 535 x 63.0
2005 Aug 19		orbit raise	91.72 167 x 550 x 63.0
2005 Aug 28	2142?	Deorbit
	2200?	Landing

Thaicom 1

 1993-078B

---

Thaicom 1 was the first lightweight HS-376L model, using a Star 30BP solid apogee motor and with a dry mass of only 436 kg. The satellite carried 644 kg of fuel at launch, with 193 kg remaining at BOL, for masses of 1080 kg and 629 kg respectively. The HS-376L satellite was 2.16m in dia, 2.6 m high at launch, with a height of 6.7 m after deployment of the solar panel skirt and antennas.

Thaicom was built for the Shinawatra Satellite Co, Bangkok, Thailand, a subsidiary of the Shinawatra Computer and Communications Group (SC&C;). It was launched as a Spelda Dedicated Satellite payload (SDS) on Ariane. The Ariane SPELDA, VEB and associated equipment had a mass of 1353 kg, and the dry mass of the H10+ third stage was 1242 kg.

In Jul 1997 Thaicom 1 was moved to 120E and renamed Thaicom 1A.

Thaicom 1
Date	Time	Event	Orbit
1993 Dec 18	0127	Launch by Ariane
1993 Dec 18	0129	PAL sep (2:21)
	0130	St 1 sep (3:32)
	0131	Fairing sep (4:31)
	0132	St 2 sep (5:44)
	0132	St 3 TIG (5:49)
	0145	St 3 MECO (18:13)
	0148	DBS 1 sep (21:37)
	0150	Mini-Spelda top sep (23:07)
	0152	Thaicom 1 sep (25:11)
	0152	H10+ sep burn (25:13)
	0156	H10+ end of mission (29:12)
	0730?	Apo 1 at 88E
	1230?	Peri 1
	1800?	Apo 2 at 71W
	2300?	Peri 2
1993 Dec 19	0500?	Apo 3 at 125E
1993 Dec 19			638.97 214 x 36177 x 3.9
	1000?	Peri 3
	1530?	Apo 4 at 33W
	2000?	Peri 4
1993 Dec 20	0200?	Apo 5 at 170E
	0700?	Peri 5
	1230?	Apo 6 at 9E
	1730?	Peri 6
	2300?	Apo 7 at 150W
1993 Dec 21	0430?	Peri 7
	1000?	Apo 8 at 48E
1993 Dec 21	0943?	Star 30BP burn	1403.92 34093 x 36215 x 0.1 GEO 49.9E+8.3E
1993 Dec 22			1378.17 33927 x 35362 x 0.4 GEO 56.4E+15.2E
1993 Dec 23	2200?	mv in
1993 Dec 26			1436.10 35771 x 35802 x 0.1 GEO 78.6E
1994 Jan 14			1436.11 35765 x 35808 x 0.1 GEO 78.5E
1997 Mar 10			1436.10 35762 x 35811 x 0.0 GEO 78.4E
1997 Jul		mv out	GEO 78E
1997 Jul 31			GEO 119E
1997 Aug 17			1436.13 35781 x 35793 x 0.0 GEO 120.0E
1999 Oct 17			1436.07 35781 x 35790 x 0.1 GEO 120.1E
2002 Aug 3			1436.11 35781 x 35792 x 0.1 GEO 120.0E

Spaceflight: August 2005

 https://welib.org/md5/d5f30d4e40ab519a5b5b2b0ef07a2a33

Gambit-3 20

  1969-019A

---

KH-8 20 was launched by Titan IIIB Agena D from Vandenberg SLC4W into a 92 degree orbit, the lowest inclination (closest to polar) flight of any KH-8 mission.

KH-8 20
Date	Time	Event	Orbit
1969 Mar 4	1930	Launch by Titan IIIB Agena D	V SLC4W
	1932?	Titan stage 1 sep
	1935?	Titan stage 2 sep
	1935?	Agena burn
	1940?	Agena MECO
1969 Mar 5	0402		90.43 132 x 459 x 92.0
1969 Mar 8	1448		89.98 128 x 417 x 92.0
		Orbit raise
	2244		90.21 121 x 448 x 92.0
		Orbit raise
1969 Mar 9	0422		90.46 127 x 466 x 92.0
1969 Mar 10	1803		90.23 130 x 440 x 92.0
		Orbit raise
	2234	90.57 136 x 468 x 92.0
		Lower perigee
1969 Mar 11	1210		90.24 114 x 458 x 92.0
1969 Mar 12	1217	Raise orbit	90.31 125 x 453 x 92.1
1969 Mar 14
	2200?	SRV recovered rev 161
1969 Mar 16	0923		89.72 132 x 388 x 92.0
1969 Mar 17	1945		89.47 125 x 371 x 92.0
1969 Mar 18		Reentered after 14d
	2145?	Deboost rev 224

The Story of Space Station Mir

 https://welib.org/md5/44690eeab3f9fa2de2ad465db1474835

Spaceflight: May 2005

 https://welib.org/md5/567abfef7087407a597c4be2c783f0a0

Monitor-E

 2005-032A

---

Launch 2005 Jul by 14A05 Rokot with Briz-KM No. 72507 from PL. The satellite, Monitor-E 98M No. 1 uses Krunichev Yacht bus, 750 kg. Krunichev is owner/operator. Box + 2 panels. Bus is 1.2 x 1.2m.

Monitor-E
Date	Time	Event	Orbit
2005 Aug 26	1834:28	Launch by Rokot	KB PL LC133/3
		T+2:26 St 1 sep
		T+3:05 GO sep
		T+5:19 St 2 sep
	1839:53	T+5:25 MES-1 dV 2229 m/s	-4000? x 250? x 97.6?
	1848:14	T+13:46 MECO-1	200? x 520? x 97.6?
	1946:12	T+1:11:44 MES-2 dV 161m/s
	1946:38	T+1:12:10 MECO-2
	2006:08	T+1:31:40 Briz sep
2005 Aug 26			524 x 544 x 97.6
	2013:48	T+1:39:20 depletion 147 m/s
2005 Aug 26		Briz orbit	147 x 538 x 97.8
2005 Oct 18		loss of attitude
2005 Nov 23		Spacecraft resumes testing
2005 Nov 26		Gamma-S first picture

Payload:

• Gamma-L 8-m camera pan, 90 km swath

• Gamma-S 20-m camera 3-band, 160 km swath

Maclean’s: July 25,2005

 https://welib.org/md5/03429978908d4196095316a7e55be733

Aviation Week: December 5,2005

 https://welib.org/md5/21b45762255c3447d892fbc851d5df95

Navstar 31

 1993-017A

---

Navstar GPS 31 (USA 90) was launched on 1993 Mar 30 from Cape Canaveral by a Delta II. The Delta also carried the SEDS experiment. SVN 31 was placed in plane C-3.

Navstar 31
Date	Time	Event	Orbit
1993 Mar 30	0309	Launch by Delta 7925	CC LC17
	0318?	T+9? Delta SECO-1	185 x 185 x 34.0
	0329?	T+20? Delta SES-2
	0329?	T+20? Delta SECO-2	184 x 746 x 34.0
	0330?	Delta/SEDS sep from GPS/PAM-D
	0331?	T+22? TES
	0333?	T+24? TECO
	0334?	T+25? PAM-D sep	357.68 185 x 20440 x 34.9
1993 Apr 1	1820?	Star 37XFP burn	723.66 20187 x 20456 x 54.9
1993 Apr 13		In service
1993 Apr 22		On station
1993 Aug 7			717.99 20071 x 20293 x 55.0
1997 Feb 1		Operating at slot C-3
2005 Oct 24		retired from service

Progress M-53

 2005-021A

---

Progress No. 353 on Mission ISS 18P. 7261 kg launch mass. Docking mass 6989 kg.

PM-53
Date	Time	Event	Orbit
2005 Jun 16	2309:32	Launch by Soyuz-U No. Zh15000-094	KB LC1-5
		T+1:59 Strapons sep
		T+3:11 Fairing sep
	2314:19	T+4:47 Blok A sep
	2314:29	T+4:57 KhO sep
	2318:17	T+8:45 Blok I MECO
	2318:24	T+8:49 Blok I sep
2005 Jun 17	0255:25	DV1 21.6m/s 54.5s
	0340:04	DV2 3.3m/s 9.5s
2005 Jun 18	0020:58	1.1m/s 4.0s
	2249:18	15.8m/s 43s
	2311:48	1.1m/s 29s
	2332:41	25.9m/s 67.2s
2005 Jun 19	0013:57	3 km, 8.1m/s 26s
	0020:13	1.1km, 4.5m/s 16.2s
	0022:27	600m, 2.3m/s 35s
2005 Jun 19		150m Comm failure, Krikalyov takes TORU control
	0041:31	Docking
2005 Sep 7	1025:57	Undocking from Zvezda
	1326:00	Deorbit 167s 87.1m/s	350 x 351 x 51.6
	1328:47	DO CO	56 x 350 x 51.6
	1405?	Reentry

Aviation Week: July 11,2005

 https://welib.org/md5/68441144ce2ca5ec15780e9358b8535a

Among the Mansions of Eden

https://welib.org/md5/7b3245bf85c9a09d98fb6ce27b7e893b

Intelsat 306

  1970-003A

---

The F-6 satellite replaced F-2 as the primary AOR satellite, but was soon replaced in turn by F-7. After a stint in 1971 as the Atlantic backup, it was moved to the Indian Ocean in 1972, and then to the Pacific in around 1974-75. It was retired in 1976 and decommissioned in 1977.

Intelsat III F-6
Date	Time	Event	Orbit
1970 Jan 15	0016:03	Launch by Delta M	CK LC17A
		Azimuth 100 deg
		SRM 1-3 sep
	0019:46	T+3:43 MECO
	0019:52?	St 1 sep
	0019:52?	SES-1 6:27
	0026:19?	SECO-1
	0041?	St 2 sep
	0042?	TES 41.6s
	0042?	TECO
	0044?	St 3 sep	631.70 267 x 35750 x 28.0
1970 Jan 16	1329	SVM-2 burn
1970 Jan 19			1436.14 35754 x 35820 x 1.0 GEO 20.6W
1970 Feb 1		AOR Primary, replaced III F-2	GEO 24W
1970 Mar 9			1436.41 35784 x 35801 x 0.9 GEO 25.1W
1970 May 4			1436.25 35784 x 35794 x 0.8 GEO 24.3W
1970 May?		Replaced by III F-7
1970 May?		AOR Backup
1970 Jun 8			1436.16 35785 x 35790 x 0.7 GEO 28.7W
1971 Jan 18			1436.46 35730 x 35857 x 0.1 GEO 30.3W+0.1E
1971 Apr		AOR Backup, moved	GEO 20W
1971 Apr 26			1434.40 35718 x 35788 x 0.2 GEO 21.9W+0.4W
1971 May 3		Move in	1436.20 35787 x 35789 x 0.2 GEO 20.1W
1972 Feb 28			1436.21 35781 x 35791 x 0.9 GEO 19.4W
1972 Mar?		Move out to IOR
1972 Jul 31		IOR	1436.21 35780 x 35797 x 1.3 GEO 64.7E+0.04E
1972 Dec 22			1436.04 35784 x 35786 x 1.7 GEO 63.1E+0.0W
1974 Dec		Move out of IOR
1975?		Move to POR
1975 Mar 14			1436.26 35780 x 35799 x 3.5 GEO 176.9W+0.05E
1975 Dec 30			GEO 182E (Morgan)
1976 Jan 15			1436.24 35782 x 35796 x 4.2 GEO 178.2W+0.04E
1976		Move out
1976 Oct 20			1436.80 35733 x 35866 x 4.7 GEO 152.1W+0.1E
1977 May 9			1435.50 35737 x 35812 x 5.1 GEO 154.2W+0.1W
1977 May 25		Orbit raise	1465.69 36185 x 36542 x 5.2

Seventeen: June 2005

 https://welib.org/md5/89edb97bcd0b7ca72ff7091fa2cd7742

MUBLCOM

 1999-026B

---

MUBLCOM (Multiple beam Beyond Line-of-sight Communications) is an experimental satellite funded by DARPA and managed by the US Army's Communications-Electronics Command (CECOM) at Ft Monmouth, New Jersey. It was built by Orbital using the Microstar (Orbcomm type) bus and carries a payload testing hand-held radio satellite communications for the armed forces.

Orbit is 750 x 750 km x 98 deg. The gravity gradient stabilized craft has a mass of 48 kg and is 0.16 long x 1.0 dia. MUBLCOM stands for Multiple Beam Beyond Line-of-Sight Communications. MUBLCOM relays packet data from user terminals to a data/voice network providing secure, mobile, terrain-independent, all-weather comms. The comms payload was developed by Torrey Science Corp. (TSC). The MUBLCOM demonstration satellite was launched in 1999. Program manager is the Space and Terrestrial Comms Directorate (S&TCD;) of CECOM, the US Army Communications/Electronics Command (part of Army Materiel Command?)

MUBLCOM also carries retroreflectors designed for use with MSFC's Advanced Video Guidance Sensor used on the DART satellite. This was not made public until DART launch preps in 2004.

The satellite was retired in 2005 Sep.

STS-74 (Atlantis)

 1995-061A

---

The STS-74 mission was the second Mir docking mission. Delivered from Atlantis to Mir were 324 kg of equipment, 147 kg of food, 450 kg of water, 20 kg of N2, and 27 kg of O2 for a total of 967 kg.. From Mir to Atlantis came 9 kg of ESA equipment, 190 kg of RKA equipment, and 171 kg of NASA equipment for a total of 371 kg. This implies a net Atlantis mass decrease of 596 kg. (The SODB data shows 313 kg down and implies 455 kg up as well as the DM; but the contemporary PAO reports seem more likely to be reliable).

STS-74 mission events
Date	Time	Event	Orbit
1995 Oct 3	0720	Roll to VAB
1995 Oct 4		Mate with ET/SRB
1995 Oct 12	0406	Roll to LC39A
1995 Nov 11		Scrub T-5m (WX)
1995 Nov 12	1230:43	Launch	KSC LC39A
	1232:47	SRB sep
	1239:17	MECO	88.29 80 x 299 x 51.7 (OMS dV)
	1239:35	ET sep
	1312:35	OMS 2 2:11 64.9m/s	90.52 294 x 305 x 51.7
	1314:46	OMS 2 CO
	1357:23	PLBD open
	1530:20	OMS-3 (R) 46s 12m/s
	1602		90.92 299 x 339 x 51.6
1995 Nov 13	0415	NC2 burn (RCS?)
	1513:55	NC3 OMS 4 40s 20m/s	91.95 346 x 394 x 51.6
	1611:44	NC4 OMS 5 (L) 38s 9m/s
1995 Nov 14	0546	RMS grapple Docking Module
	0637	Unberth DM
	0716	Berth DM to ODS with RCS
	0900	RMS ungrapple DM
	0941	HO to DM
	1519	NC4 RCS 21s 1.5m/s	92.00 350 x 394 x 51.7
1995 Nov 15	0153:04	NC5 OMS-6 (R) 33s 8m/s	92.29 379 x 394 x 51.6
	0326:43	OMS-7 (L) TI 9s 3m/s	92.39 387 x 396 x 51.7
	0528	Rendezvous at 50m
	0556	Resume approach
	0618	Stationkeep at 10m
	0622	Resume approach
	0627:39	Dock DM with Kristall
	0636	APDS retracted and latched
	0900	DM hatch open	92.42 391 x 395 x 51.6
	1130?	DM control to Russia
1995 Nov 16	0526	RCS Orbiter/Mir structural dynamics test
1995 Nov 17	1746	Crew return, hatch closed
1995 Nov 18	0815:44	Atlantis undock from DM	92.42 391 x 395 x 51.6
	0832	Stationkeep at 120 m, begin flyaround
	0915?	Second flyaround
	1005	Sep burn	92.39 388 x 395 x 51.6
	1514:20	OMS 8L 47s 13m/s lower orbit for GLO
	1558:03	OMS 9R 55s 15m/s	91.39 337 x 348 x 51.6
1995 Nov 19	1134	DTO 829 plume test RCS
	1841	GLO RCS burns begin
	1914	GLO RCS burns end
1995 Nov 20	1320	PLBD closed	91.36 336 x 346 x 51.6
	1558:43	OMS deorbit 3:54 132.2m/s	-106 x 346 x 51.6
	1602:37	OMS DO CO
	1630:02	Entry interface 122km
	1701:09	Gear down
	1701:27	MGTD RW33 KSC
	1701:37	NGTD
	1702:24	Wheels stop
	1955	Tow to OPF/1

Back in Black

 https://welib.org/md5/b1e3cf8bdfa7a822d2dafc3bf30f2e1d

Space stations : base camps to the stars

 https://welib.org/md5/f6dd4b668d6fe0310d72cbf598498a4f

Seventeen: July 2005

 https://welib.org/md5/b7f19d75982fe789f06c46e94410fd4f

History of Sunnehanna Country Club (1923-2004)

 https://welib.org/md5/3eff7688d81585c93b65119a1cd46b3d

Star-crossed orbits : inside the U.S.-Russian space alliance

 https://welib.org/md5/d20ea1a0e4885dd1b2b7448a31b14baf

Explorer 42

  1970-107A

---

The first small Explorer payload, SAS-A, carried two x-ray proportional counters provided by the American Science and Engineering team which later became the x-ray astronomy group of the Smithsonian Astrophysical Observatory. It was launched at 1053 on 1970 Dec 12 by a Scout B from the San Marco Launch Complex in the Indian Ocean off Kenya. It reached a 95.30 min, 522 x 563 km x 3.04 deg orbit and began operations on Dec 18. SAS-A was given the designations Small Astronomy Satellite 1 (SAS 1) and Explorer 42, but it is famous by the name given to it in honor of the Kenya-based launch site - Uhuru, the Swahili for `freedom'. Uhuru was the first successful x-ray astronomy satellite and made a survey of the 2-10 keV x-ray sky which was turned into a series of catalogs, the final one being the Fourth Uhuru (4U) catalog. Uhuru operations ended on 1973 Mar 18 and the satellite reentered on 1979 Apr 5.

Uhuru
Date	Time	Event	Orbit
1970 Dec 12	1053:50	Launch by Scout B S175C	SMLC
		T+1:16 St 1 burnout
		T+1:19 Stage 2 burn
		T+1:59 Stage 2 burnout
		T+2:13 Stage 3 burn
		T+2:49 Stage 3 burnout
		T+9:05 spinup
		T+9:07 Stage 3 sep
	1103:02	T+9:12 Stage 4 burn
	1103:37	T+9:47 Stage 4 burnout
	1108:17	T+14:27 Stage 4 sep
		Magnetic despin
1970 Dec 13			95.76 535 x 574 x 3.0
1971 Feb		Tape recorder failed
1971 May 25			95.63 530 x 568 x 3.0
1971 Aug		Transmitter strength weakened
1971 Sep		Degraded star sensors
1971 Dec		Transmitter recovered
1972 Mar		Battery failed, day ops only
1973 Mar 18		End of ops

Wolves in Chic Clothing

 https://welib.org/md5/93a87794a543fe8707d5e5d3f799eef9

Anik E2

 1991-026A

---

Anik E-2, the first Anik E to be launched, left the South American launch pad in Apr 1991. 8 days later on Apr 12 the C-band antenna failed to deploy, but finally on Jul 3 the antenna was successfully released. In Sep 1991 E-2 replaced the Anik C-1 Ku-band satellite.

In Jan 1994 a magnetic storm caused the momentum wheel assembly to fail, and the spacecraft was feared lost. Services were transferred to other satellites. However, control was regained in Jun 1994 using a ground based computer to control attitude thruster firings. 

Anik E-2
Date	Time	Event	Orbit
1991 Apr 4	2333:00	Launch by Ariane 44P V53	CSG ELA2
		T+1:09 PAL sep
		T+3:32 St 1 sep
		T+3:34 St 2 MES
		T+4:27 Fairing 01 sep
		T+5:43 St 2 sep
	2338:46	T+5:46 St 3 MES
	2350:47	T+17:47 St 3 MECO
	2352:42	T+19:43 St 3 sep	636.35 451 x 35805 x 4.0
1991 Apr 5	1540?	LAM-1	724.50 4907 x 45778 x 1.8
1991 Apr 6	1500?	LAM-2	918.11 14077 x 35748 x 0.7
1991 Apr 8	1330?	LAM-3	1090.64 21692 x 35747 x 0.2
1991 Apr 10	0150?	LAM-4	1195.52 26119 x 35751 x 0.3
1991 Apr 11	1800?	LAM-5	1434.56 35715 x 35797 x 0.0 GEO 109.3W+0.4E
1991 Apr 25			1432.26 35671 x 35751 x 0.1 GEO 98.1W+1.0E
1991 Jun 11			1435.30 35749 x 35792 x 0.3 GEO 81.5W+0.2E
1991 Jul 31		mv in	1436.05 35779 x 35791 x 0.1 GEO 108.6W
1991 Sep 1		Replaced Anik C-1
1991 Sep 28			1436.09 35777 x 35795 x 0.0 GEO 107.3W
1993 Jan 26			1436.10 35777 x 35795 x 0.0 GEO 107.4W
1994 Jan 21		Attitude control failure
1994 Mar 1			1436.11 35777 x 35796 x 0.1 GEO 107.4W
1994 Jun 21		Attitude control regained
1994 Aug		Restored to service
1994 Oct 19			1436.09 35780 x 35792 x 0.0 GEO 107.3W
1996 Sep 5			1436.08 35776 x 35796 x 0.0 GEO 107.3W
1999 Jun 10			1436.08 35777 x 35795 x 0.0 GEO 107.3W
2001 Feb 19			1436.16 35774 x 35801 x 0.1 GEO 107.3W
2001 Feb		Move to 111W
2001 Feb 27			1436.14 35783 x 35791 x 0.1 GEO 111.1W
2003 Jun 27			1436.09 35776 x 35796 x 0.1 GEO 111.1W
2003 Jul 7			GEO 111W
2003 Jul 23		Move to 119W	GEO 119W
2003 Sep 6			1436.12 35768 x 35805 x 0.2 GEO 118.7W
2005 Mar 29			1436.01 35766 x 35803 x 1.7 GEO 118.5W

Opera: A Research and Information Guide, 2nd Edition

https://welib.org/md5/7f81cc095070cb195c849cd83e8294e5

Thuraya 2

 2003-026A

---

Boeing GEM launched Jun 2003 by Boeing for Thuraya/Abu Dhabi, to supplement T-1 at 44E. T-3 to follow.

5177 kg launch, 3200 kg BOL. Size is box + 2 panels 7.6 x 3.2 x 3.4m with 40.4m span. T-2 has longer arrays that T-1 with no solar concentrators.

Planned inclination is 6.3 deg at 44E.

Thuraya 2
Date	Time	Event	Orbit
2003 Jun 10	1355:59.2	Launch by Zenit-3SL	Odyssey
		T+2:24 St 2 MES
		T+2:29 St 1 sep
	1359:44	T+3:45 Fairing sep
	1404:31	T+8:32 St 2 sep	-2155 x 187 x 6.3
	1404:39	T+8:40 DM MES-1
	1409:57	T+13:38 DM MECO-1	180 x 1390 x 6.3
	1510:41	T+1:14:42 DM MES-2
	1515:58	T+1:20:59 DM MECO-2
	1535:18	T+1:40:19 DM sep	649.54 1177 x 35755 x 6.2
2003 Jun 11			650.79 1207 x 35788 x 6.3
2003 Jun 12		LAM-1	759.15 6604 x 35772 x 6.3
2003 Jun 16		LAM-2	1259.69 28752 x 35764 x 6.3
2003 Jun 17	0830?	LAM-3	1388.62 33920 x 35783 x 6.3
2003 Jun 19		LAM-4	1436.01 35747 x 35822 x 6.3 GEO 28.7E+0.0E
2003 Jul 28			1436.09 35711 x 35861 x 6.2 GEO 28.8E

Town and Country: February 2005

 https://welib.org/md5/92ba34d88418c3ae37d9b51ec0d65ff1

Apollo 11 (Eagle)

  1969-059C

---

The first spacecraft to carry humans to a landing on another world was Lunar Module 5, the spaceship Eagle.

On 1969 Jul 20, Eagle landed at Tranquility Base, 00 41 15 N, 23 26 00 E, later given the official astronomical name Statio Tranquillitatis, in the Mare Tranquillitatis, Luna.

During the descent, computer program alarms occupied the crew, preventing them from noticing the rough terrain the automated descent was leading them towards. Armstrong took over manual control with three and a half minutes of fuel left, and flew Eagle around until he found a safe spot, landing with only 45 seconds of fuel left and 25 seconds from the abort decision point.

Eagle (LM 5)
Date	Time	Event	Orbit
1969 Jul 16	1332	Launch by Saturn V (SA-506)	KSC LC39A
	1749:03	Extract from S4B-506 by CSM 107
1969 Jul 18	2100	Hatch open, first crew entry
1969 Jul 20	1300	Crew entry
	1744	Undocked from CSM 107	100 x 122
	1908:14	DPS DOI-1 (0:30) 23m/s	16 x 106
	1908:44	DOI-1 cutoff
	2004	At 15 km
	2005:05	DPS PDI
	2008	Yaw LM to face-up
	2010:22	1202 program alarm
	2010:50	At 10 km altitude
	2011:02	1202 alarm
	2013:32	Program P64 2.2km, high gate
		Approach phase
	2013:43	Attitude hold
	2014:18	1201 alarm
	2014:19	Below 750m
	2015:22	P-66, manual control
		150m, low gate
		Landing phase
	2017:40	Landed at Tranquility Base
1969 Jul 21	0227	LEVA-1 begin depress
	0230	Pressure at 0.4psi
	0238	Depress complete
	0239	Hatch open
	0249	Cdr egress
	0256	Cdr to lunar surface
	0311	LMP egress
	0315	LMP on surface
		Deploy EASEP
	0503?	LMP return after 01:47
	0510	Cdr return after 02:20
	0511	Hatch closed
	0514	Repress
	0740:12	Depress for equipment dump 114:08:12
	0742?	HO?
		Dump LiOH canister, 2 PLSS, 2 LM arm rests
	0744?	HC
	0745	Repress
	0750	Repress complete

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LM 5
Date	Time	Event	Orbit
1969 Jul 21	1754:01	Launch from LM 5 DS, Tranquility Base
		APS burn 7:15
		Residual trim complete 8:37
	1801:21	LOI	17.6 x 87.6
	1851:34	RCS CSI (0:45)	84 x 90
	1852:22	RCS CSI cutoff
	1949:50	RCS CDH (0:18)	76 x 87
	2035:52	TPI (0:23)	81 x 113
	2036:14	TPI cutoff
	2051:25	MCC1 midcourse
	2106:58	MCC2 midcourse
	2111:34	TPF (0:28)	105 x 115
	2117	Rendezvous with CSM 107
	2135:00	Docked with CSM 107
	2145	Crew and cargo transfer
	2342	Undocked from CSM 107
1969 Jul 22	0425?	end of ops

Kosmos 2414

 2005-002A

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Parus satellite launched in early 2005. The satellite was launched using a Kosmos-3M with a special fairing designed for the SAR-Lupe satellites. This flight qualified the fairing, which has bulges on the side to contain the SAR-Lupe antenna; the heavier fairing meant Parus was targeted at a lower orbit than usual.

Kosmos-2414
Date	Time	Event	Orbit
2005 Jan 20	0300:07	Launch by Kosmos-3M	PL 132/1
	0302	Stage 2 burn
	0308?	Stage 2 MECO-1
	0401?	Stage 2 MES-2
	0401?	Stage 2 MECO-2
	0402	Sep from stage 2	912 x 966 x 83.0
	0402?	Universitetskiy sep
2005 Jan 27			103.80 909 x 966 x 83.0