Progress M-28

 1995-036A

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Progress 228 was launched on 1995 Jul 20, with mass 7125 kg at launch. It carried 400 kg of experiments (347 kg of them for ESA), 400 kg of water and 306 kg of food.

Progress M-28
Date	Time	Event	Orbit
1995 Jul 20	0304:41	Launch by Soyuz-U	LC1
	0313:30	Blok-I sep	88.69 191 x 258 x 51.6
	0647:29	TCM-1, dv 20 m/s
	0736:50	TCM-2, dv 13 m/s	89.83 246 x 308 x 51.6
1995 Jul 21	0406s	TCM-3
1995 Jul 22	0439:37	Docked with Mir -X
1995 Sep 4	0509:53	Undocked from -X
	0814:20	Deorbited E of New Zealand
	0858:55	Reentered

The official celebrity registry, 1993-1994

https://welib.org/md5/c654571780a921d13b9f4bbd80a6cf47

Kosmos 636

  1974-016A

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Kosmos-636 flew a 2 week mission at 65 degrees from Baikonur in Mar 1974.

Kosmos-636
Date	Time	Event	Orbit
1974 Mar 20	0830	Launch by 11A57	KB
	0834	Blok-I burn
	0838	Blok-I sep
	1722		90.03 165 x 386 x 65.0
1974 Mar 21	0700		90.02 165 x 396 x 65.0 (RAE)
	0652		90.01 164 x 385 x 65.0
		Lower orbit
	1200		89.26 167 x 309 x 65.0 (RAE)
	1250		89.25 166 x 308 x 65.0
		Adjust perigee
1974 Mar 24	0319		89.25 170 x 304 x 65.0
1974 Mar 28	1551		89.12 168 x 293 x 65.0
1974 Apr 1	1449		88.92 167 x 274 x 65.0
1974 Apr 2		Engine sep	90.57 184 x 422 x 65.0
1974 Apr 3	0517?	Retrofire
	0527?	PO sep
	0531?	Entry
	0548?	Landed after 13.9d

Progress M-36

 1997-058A

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Launch mass was 7195 kg. After undocking, Progress M-36 released the Inspector satellite. Finally, Progress M-36 tested out two new model DPO auxiliary engines. Orlan M-6 was delivered. Orlan DMA-25 was jettisoned, according to Suzy McHale's site.

Progress M-36
Date	Time	Event	Orbit
1997 Oct 5	1508:57	Launch by Soyuz-U	KB LC1
	1512	Blok-I burn
	1517:46	Blok-I sep
	1850:02	TCM-1
	1942:34	TCM-2	241 x 316 x 51.7
1997 Oct 6	1713:51	TCM-3
1997 Oct 7	1442:22	TCM-4
	1509:06	TCM-5
1997 Oct 8	1707:09	Docking at Kvant using Kurs system
1997 Dec 17	0601:53	Undocked
	0606:30	Sep burn
	0655:00	Stationkeep burn at 700m
	0735:00	Deploy Inspector
	1211:30	Sep-2 burn
1997 Dec 19	0522	DPO engine burn, 1500s	229 x 374 km
1997 Dec 20	1320:01	Deorbit burn 1:41, 49m/s
	1401s	Reentered

Aviation Week: October 5,1998

 https://welib.org/md5/e72ac9a3af85a652c9c67217951e88f0

A Journey In Other Worlds

 https://www.gutenberg.org/files/1607/1607.txt

Aviation Week: November 9,1998

 https://welib.org/md5/f4f3e1a519069eaf182d024f5903cf3d

Demosat

 1999-014A

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The SeaLaunch Zenit-3/Blok DM-SL was be launched from 0 N 154 W on its first mission. Stage 1 will impact 147W 0N, Stage 2 at 111W 0N.

Stage 1 is 33m long 3.9m dia. The RD-171 had four thrust chambers with 739 kNs thrust. Stage 2 is 10.4m long, with a single chamber RD-120 with 94 kN thrust and an RD-8 vernier with 8kN thrust, all LOX/kero. The DM-SL is 5.6m long 3.7m dia with an 8.0kN 11D58M engine.

The demo launch in 1999 Mar will use an inert pathfinder payload representing an HS-702. The square truss with four mass booms eproduces the dynamic properties of Galaxy 11. The payload was built at Boeing/Kent and has a mass of 4700 kg. 

DemoSat
Date	Time	Event	Orbit
1999 Mar 28	0129:59	Launch from SL Odyssey
		T+2:26 Stage 1 sep
		T+3:20 Fairing sep
		T+9:05 Stage 2 sep	-2200? x 204 x 1.3?
	0139:15	T+9:15 Blok DM-SL burn 1
	0143:46	T+13:46 Blok DM-SL MECO-1, EPO	93.74 180 x 735 x 1.3
	0217:20	T+47:20 DM-SL burn 2
	0223:20	T+53:20 DM-SL MECO-2	720 x 36536 x 1.3
	0231:40	T+1:01:40 DM-SL sep
	0517	T+3:47 DM-SL disposal burn
		T+3:52 CCAM burn end	641.77 597 x 35938 x 1.3

USA-106

 1994-057A

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Block 5D-2 S-11 (DMSP 23545, USA 106) was launched by Atlas 20E from Vandenberg in Aug 1994. It became flight F-12.

DMSP 23545 (S-11)
Date	Time	Event	Orbit
1994 Aug 29	1738	Launch by Atlas 20E	V SLC3W
	1740	T+2:04 Booster sep
	1740	T+2:24 Fairing
	1743	T+5:21 SECO
	1743	Atlas sep
	1748?	T+10:27 Star 37S burn
	1749?	Star 37S burnout
	1749?	T+11:43? Orbit trim
1994 Aug 29			101.94 842 x 859 x 98.92
1994 Sep 2			101.95 842 x 859 x 98.9