September 13,2008

 https://en.wikipedia.org/wiki/Congregation_Baith_Israel_Anshei_Emes

Perfect couple : a Superlatives novel

 https://welib.org/md5/964541a180c1e5a2ffafeb8fd489d43f

ATV-5 (Georges Lemaitre)

 2014-044A

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2682 kg dry cargo, 6600 kg total cargo. 19926 kg launch mass plus 134 kg adapter; 9778 kg dry. 16380 kg at undocking, departing with 2690 kg prop, 2147 kg dry cargo, 353 kg liquid cargo.

ATV5
Date	Time	Event	Orbit
2014 Jul 29	2347:38	Launch by Ariane 5ES
		T+2:17 EAP sep
		T+3:26 Fairing sep
	2356:19	T+8:41 EPC MECO	-1249 x 141 x 51.2
	2356:25	T+8:47 EPC sep
	2356:31	T+8:53 EPS burn 1	137? x 260?
2014 Jul 30	0004:43	T+17:05 EPS MECO 1
	0046:34	T+58:56 EPS MES2 55s
	0047:25	T+59:51 EPS MECO2
	0051:27	T+1:03:49 ATV sep	89.70 252 x 267 x 51.6
		T+1:04:05 ADM burn to sep EPS
	0211:55	T+2:24:17 EPS deorbit
	0918:58	TPO burn 21.2m/s
	1007:22	TPO burn 21.3m/s (285 kg in 2 burns)
2014 Aug 1		CAM test burn
2014 Aug 2	0942:11	MCI burn 34s, 1.77m/s)
	1020:43	MCI burn 33s 1.75m/s)25 kg
2014 Aug 5	1235:24	MCI burn 187s 1.4m/s)
	1320:03	MCI burn 186s 1.4m/s ) 43kg
2014 Aug 7		TIV burns set 1
2014 Aug 8		TIV burns set 2
	2107:04	S-1/2 Fly-under of ISS
2014 Aug 10	0319:02	DV 62s 3.3m/s
	0404:54	DV 99s 5.2m/s
	0450:42	DV 177s 1.38m/s
2014 Aug 11	1655:49	TV burn 4.0m/s
	1747:20	burn 8.1m/s
	1844:10	burn 2.9m/s
	2245	Flyunder, closest approach, 6.1km range
		Test of LIRIS lasers
2014 Aug 12
	0153	burn 2.5m/s
	0240	burn
	0922	S-1/2 burn at 39 km
	1205	Hold at S3, 249m
	1243	Depart S3
	1305	Hold at S4, 19m
	1321	Rendezvous 11m skeep
	1329:53	Docking Zvezda
2014 Aug 14	1658:00	OCS reboost ISS 469s 1.1,/s 151.6 kg
2014 Aug 27	0837	OCS reboost ISS, 2:58 0.43m/s 179s 59 kg
2014 Sep 14	0208:00	Reboost 224s 0.55m/s 88 kg
2014 Oct 8	0913	Reboost ISS 515s 1.22m/s 187 kg
2014 Oct 27	1742:04	PDAM 34881, reboost 0.5m/s, 203s
2014 Nov 12	1235	PDAM 39372 3:25
2015 Jan 28	1840:00	ATV OCS deboost ISS for phasing; 4:49 0.7m/s
2015 Feb 14	1342	Undocked from Zvezda
	1348?	Sep burn
2015 Feb 15
	1429:29	DEO1 Orbit lowering burn 13:46 51.7m/s	207 x 404 x 51.7
	1443:15	DEO 1 CO
	1726:01	DEO2 Deorbit burn 23:18 1398s 89.6m/s
	1749:18	DEO2 CO
		100 km reentry
	1812s	impact

Astra 2B

 2000-054A

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Astra 2B will be launched in 2000 to 28.2E. It is a Astrium (Matra Marconi Space) Toulouse Eurostar 2000+ satellite. Mass is 3315 kg launch, 1511 kg BOL. Astra 2B will replace the DFS Kopernikus system.

Size is 2.8 x 1.7 x 2.5m with 32m span.

Astra 2B
Date	Time	Event	Orbit
2000 Sep 14	2254	Launch by Ariane 506 V130	CSG ELA2
		T+0:00 EPC burn
		T+7:00 EAP ignition
		T+7:03 Launch
		T+2:25 EAP sep
		T+3:22 Fairing sep
	2304	T+9:57 EPC MECO
	2304	T+10:03 EPC sep	50? x 1500? x 7?
	2304	T+10:10 EPS burn
	2321	T+27:17 EPS MECO
	2322	T+28:42 Astra sep
	2324	T+30:28 Sylda 5 sep
	2327	T+37:39 GE 7 sep
		T+54:08 EPS depleted
2000 Sep 15			637.59 568 x 35752 x 7.0
2000 Sep 16			959.36 15911 x 35775 x 1.6
2000 Sep 19			1318.77 31153 x 35762 x 0.3
2000 Oct 2?		mv in
2000 Oct 10			1436.12 35777 x 35797 x 0.1
2000 Oct 23			1438.23 35825 x 35831 x 0.1 GEO 28.9E
2000 Nov 20			1435.97 35768 x 35800 x 0.0 GEO 28.6E
2006 Jul 28			1436.16 35779 x 35796 x 0.0 GEO 28.2E
2013 Feb 6			1436.11 35777x 35795 x 0.0 GEO 28.2E
2013 Feb 6		Move out
2013 Feb 26		Move in	1436.11 35769 x 35804 x 0.1 GEO 19.4E
2014 Jan 15			1436.07 35769 x 35802 x 0.1 GEO 19.4E

USA-191

 2006-050A

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The S-17 spacecraft, F-17 mission was launched by a Boeing Delta 4 from Vandenberg. Target orbit was 1734LT SSO.

A large number of debris objects were cataloged associated with the Delta 4 deorbit burn.

DMSP F-17
Date	Time	Event	Orbit
2006 Nov 4	1353	Launch by Delta IVM	V SLC6
		Azimuth 189.5
		T+4:04 MECO
		T+4:11 Stage 1 sep
		T+4:26 SSIC-1
		T+4:36 Fairing sep
		T+14:37 Positive perigee
	1407:58	T+14:58 SECO-1	846 x 850 x 98.8
	1411:18	T+18:18 Stage 2 sep
	1411	Delta stage debris?
		T+41:55 Perigee 1
	1544	T+1:51:43 SSIC-2
	1547	T+1:54:37 SECO-2, depletion	-4009 x 2297 x 98.77
	1550	T+1:57:00 Stage 2 breakup
		T+2:01:08 Stage 2 debris impact
2016 Jan		Secondary sat