Kosmos 295

 1969-073A

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DS-P1-Yu No. 29, was a Subgroup 1 mission which overlapped with Kosmos-285. 

Kosmos-295
Date	Time	Event	Orbit
1969 Aug 22	1415	Launch by 11K63	PL
	1417	Stage 2 burn
	1422?	Stage 2 sep
1969 Aug 28	0230		91.95 270 x 469 x 71.01
1969 Sep 27		end of ops
1969 Oct 11	0350?	Stage 2 reentered
1969 Dec 1	1800?	Reentered

Kosmos 859

 1976-099A

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Kosmos-859
Date	Time	Event	Orbit
1976 Oct 10	0935	Launch by Soyuz-U	Baikonur
	0939	Blok-I burn
	0943	Blok-I sep
1976 Oct 10			89.60 171 x 337 x 65.0
1976 Oct 11			89.59 171 x 336 x 65.0
1976 Oct 12			89.37 171 x 314 x 65.0
1976 Oct 15			89.30 170 x 308 x 65.0
1976 Oct 16			89.34 169 x 314 x 65.0
1976 Oct 18			89.29 169 x 309 x 65.0
1976 Oct 19			89.34 167 x 315 x 65.0
1976 Oct 20			89.31 168 x 312 x 65.0
1976 Oct 21
	0555?	Deorbit
	0605?	PO sep
	0609?	Entry
	0625?	Landed

Jindai

 1986-061C

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The first H-1 test flight used a two-stage variant. The first stage used a Thor MB-3 engine with nine Nissan solid motors. The second stage was the LE-5 liquid engine. Attached to the LE-5 was a small rectangular box, the MABES (Magnetic Bearing Flywheel Experimental System) experiment. MABES was operated to test attitude control technology and was built by the National Aerospace Lab in Tokyo (NAL). It was named Jindai after launch, Jindai being a kind of cherry tree. Jindai measured a 2-axis magnetic bearing flywheel spinning at 1000 rpm and tested a 400 x 500 pixel CCD star sensor and a linear array sun sensor. The box contained a quartet of NiCd batteries and the spacecraft operated on and off for 3 months.

Jindai (MABES)
Date	Time	Event	Orbit
1986 Aug 12	2045:00	Launch by H-1	TNSC
		SOB sep
	2047	Stage 1 sep, LE-5 on at 114 km (T+2:39)
	2055	Stage 2 cutoff (T+10:13), transfer orbit	200? x 1487 x 50.0
	2139	LE-5 restart, 21s (T+54:33)
	2140	LE-5 cutoff	1485 x 1594 x 50.0
	2142?	Ajisai sep
	2145?	Fuji sep
1986 Nov 8	1230	end of ops
1994 Aug 23			115.71 1478 x 1496 x 50.0