Saturn S-IVB-506

  1969-059B

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SA-506 was launched at 1332:00 on 1969 Jul 16 on the Apollo 11 mission. The S-IVB reignited for the TLI burn at 1616. Apollo 11 separated at 1749. S-IVB-506 passed the Moon at 4334 km on 1969 Jul 19 at 2022:34 and entered a solar orbit of 134.30 x 151.86 Mkm x 0.38 deg, 342 days.

SA-506
Date	Time	Event	Orbit
1969 Jul 16	1332:00	Launch by Saturn V (SA-506)	KSC LC39A
	1334:15	S-IC CECO, 44.4 km
	1334:41	S-IC OECO, 66.3 km
	1334:42	S-IC sep, 67.0 km
	1334:43	S-II ignition, 67.6 km
	1335:12	Interstage sep, 91.8 km
	1335:18	LES sep
	1336:29	S-IC apogee, 115 km	-5998 x 114 x 32.1
	1339:40	S-II CECO, 179.3 km
	1341:03	S-IC impact, 30.21N 74.04W
	1341:11	S-II OECO, 185.9 km
	1341:12	S-II sep, 185.9 km	-2112 x 189
	1341:15	S-IVB burn 1 ignition, 185.9km
	1341:21	Ullage case jettison
	1341:47	S-II apogee, 189 km
	1343:42	S-IVB cutoff, 188.4 km
	1343:49	Earth orbit insertion	88.18 183 x 196 x 32.52
	1352:14	S-II impact, 31.54N 34.84W
	1616:27	S-IVB TLI burn (5:47)
	1622:03	S-4B MECO-2
			224 x 527965 x 31.39 (V)
			224 x 529545 x 31.39 (C3)
	1622:13	Translunar injection
			222 x 564184 x 31.38 (V)
			224 x 566485 x 31.38 (C3)
	1647:23	CSM sep from LM/S-IVB
	1656:03	CSM docked with LM/S-IVB
	1749:03	CSM/LM undocked from S-IVB
	1823:08	CVS LH2 vent 7.3m/s
	1835:07	LOX dump 180s 17m/s
	1836:55	LOX dump end
	1857:00	H2 NPV
	1909:47	APS burn 280s 12m/s
	1914:27	APS cutoff
1969 Jul 19	2022?	Lunar flyby at 3379 km altitude

Helios 1

  1974-097A

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The Helios solar probes were a joint project between DFVLR and NASA, which provided the Titan Centaur launch vehicle.  Helios 1 was launched on 1974 Dec 10 by Titan IIIE Centaur from Cape Canaveral's Launch Complex 41. Two Centaur burns placed the Helios probe in solar orbit. The Centaur TC-2 stage then made two retrograde test burns, which happened to leave it in an orbit bound to the Earth - it thus became the first object known to have returned to Earth orbit from a solar orbit trajectory with the possible exception of Apollo lunar spacecraft. NORAD cataloged two objects in a 1765 x 157261 km x 31.8 deg orbit; object D, the second object, may be a duplicate of the first or may represent some kind of debris from the Centaur after venting. However, the name of the object was later changed to 'Helios 1 debris' and with its elements marked in the Satellite Situation Report as 'heliocentric orbit', it may be the Star 37E tumble weight.

Helios 1
Date	Time	Event	Orbit
1974 Dec 10	0711:01	Launch
		T+1:40 Forward bearing reactor sep
		T+1:51 Stage 1 MES
	0713:05	T+2:04 SRM sep
		T+4:18 Stage 1 MECO
	0715	T+4:19 Titan stage 1 sep
	0715	T+4:19 Stage 2 MES
	0716	T+5:18 Fairing
	0718:50	T+7:49 St 2 MECO 165 km 7.01 km/s
	0718:53	T+7:52 Titan stage 2 sep	-1950? x 165 x 29.9
	0719:04	T+8:03 Centaur TC-2 MES1, 100.8s
	0720:42	T+9:44 Centaur TC-2 MECO1, start 21.9 min coast
	0726?	Stage 2 reentry
	0742:40	T+31:39 Centaur TC-2 MES2, 276s,
	0747:14	T+36:13 Centaur MECO-2 255 km?
		T+37:23 Spinup
	0748:26	T+37:25 Centaur TC-2 sep from Helios 1/Star 37
		Clamp band halves separate
	0748:26	T+37:25 TC-2 retro
	0749:06	T+38:05.76 Star 37E burn, 44.90s (action time 43.6s)
	0749:51	T+38:50.66 Star 37E burnout 528 km	289 x -21954 x 29.80
		Payload clamp band
	0751:02	T+40:01 Star 37E sep	Solar orbit 180d, 0.30958 x 1.0 AU x 0.016
	0751:06	T+40:05 Yo deploy
	1156	Helios/Star 37 pass EL1:4
	1654	Centaur clamp pass EL1:4
1974 Dec 12	0330?	Helios/Star 37 exit Earth sphere (L1)
1974 Dec 15	1200?	Centaur clamp band exit Earth sphere
1975 Feb 15	0915	Perihelion, 0.30AU
1976 Mar 29		Perihelion 3
1976 Jul 2		Aphelion 3
1982		Still operating

Payload:

• E1 Solar wind plasma expt (MPE/Rosenbauer)

• E2 Fluxgate magnetometer (TU Braunschweig/Musmann)

• E3 Fluxgate magnetometer (GSFC/Ness)

• E4 Search coil magnetometer (Braunschweig/Dehmei)

• E5 32 m antenna for plasm and radiowave expt, 50 kHz-2 MHz (Iowa/Gurnett)

• E6 Cosmic ray expt (Kiel/Kunow)

• E7 Cosmic ray expt (GSFC/Trainor)

• E8 Electron detector (MPIA-Lindau/Keppler)

• E9 Zodiacal light photometer (LSW-Heidelberg/Leinert)

Kosmos 1424

 1982-117A

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Kosmos-1424
Date	Time	Event	Orbit
1982 Dec 16	1000	Launch by Soyuz	Baikonur
	1008	Blok-I sep
1982 Dec 16			89.73 172x351x64.9
1982 Dec 22			89.30 172x308x64.9 from 89.25 165x311
1982 Dec 25			89.67 168x349x64.9 from 88.94 166x279
1982 Dec 29		SpK-1 fid
1982 Dec 30			89.59 163x346x64.9 from 89.35 162x323
1983 Jan 5			89.56 173x333x64.9 from 88.97 154x293
1983 Jan 11			89.60 168x342x64.9 from 88.68 162x257
1983 Jan 13		SpK-2 fid
1983 Jan 24			88.83 165x269x64.9
1983 Jan 28
	2112?	Deorbit
	2128?	Entry
	2140?	Landed

Progress 13

 1982-047A

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The first cargo ferry launched to Salyut-7 was 11F615A15 No. 114 (7K-TG No. 114), announced as Progress-13. 

Progress-13
Date	Time	Event	Orbit
1982 May 23	0556:41	Launch by Soyuz-U	KB
	0605	Blok-I MECO
	0610		88.99 186 x 263 x 51.6
	1430		90.85 286 x 347 x 51.6
1982 May 24	0930		90.90 291 x 347 x 51.6
1982 May 25	0756:36	Docked with Salyut-7
1982 May 26			91.35 338 x 344 x 51.6
1982 Jun 4	0631	Undocked
1982 Jun 5			90.75 307 x 316 x 51.6
	0500		90.62 304 x 307 x 51.6
	0930		89.03 214 x 240 x 51.6
	1200		89.02 215 x 238 x 51.6
1982 Jun 6	0005	Deorbited over Pacific

Globalstar 2

 1998-023A

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Second launch of four sats on Delta 256.

Globalstar FM14
Date	Time	Event	Orbit
1998 Apr 24	2238:34	Launch by Delta 7420-10	CC LC17A
	2239	T+1:03 SRM 1-4 burnout
	2239	T+1:06,1:07 SRM 1-2, 3-4 sep
	2242	T+4:24 MECO
	2243	T+4:32 St 1 sep
	2243	T+4:37 St 2 burn
	2243	T+4:47 Fairing sep
	2249	T+11:22 SECO 1	185 x 1241 x 52.0
	2339	T+1:01:14 Stage 2 burn 2
	2340	T+1:01:3 SECO-2	1247 x 1247 x 52.0
	2346	T+1:08:20 FM5,6 sep
	2350	T+1:12:30 FM7.8 sep
		SECO-3 sep
1998 Apr 25	0033:34	SECO-4 depletion
1998 May 11			111.61 1273 x 1327 x 52.0
1998 May 22			114.09 1389 x 1438 x 52.0
1998 Jun 16			114.08 1398 x 1428 x 52.0
1998 Nov 16			114.08 1411 x 1415 x 52.0
2001 Sep 26			114.08 1412 x 1414 x 52.0

Young Miss: November 2001

 https://welib.org/md5/d4f9860ad2fdd54e54a759630b0b544d