BSat 2A

 2001-011B

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BSat 2a and 2b will be Orbital Star (NovaStar) 550 kg (dry) lightsats. They will provide HDTV digital broadcasting from the 110E slot.

BSat-2a is underneath Sylda. Mass is 1317 kg launch, 535 kg dry. Size is 3.8 x 2.5 x 2.0m with 16.1m span.

The EPC orbit of 243 x 1884 km given in the EADS press kit is probably a typo for 43 x 1884 km.

According to C. Niederstrasser of Orbital the satellite was decommissioned in Jan 2013, 1.5 years after being sent to the GEO graveyard; presumably there was interest in studying the long term surivival of the first of this class of spacecraft.

Bsat-2A
Date	Time	Event	Orbit
2001 Mar 8	2251	Launch by Ariane 5G	CSG ELA3
		T+2:25 EAP sep
		T+3:14 Fairing sep
		T+9:40 EPC MECO
	2300	T+9:46 EPC sep	43? x 1884 x 6.7
	2300	T+9:53 EPS burn 200 km
	2317	T+26:37 EPS MECO
	2320	T+29:13 Eurobird sep
	2323	T+32:29 Sylda 5 sep
	2327	T+36:21 BSAT-2a sep
2001 Mar 9	0033?	EPC reentry
2001 Mar 9			642.69 897 x 35685 x 2.23
2001 Mar 10	0155?	AKM
2001 Mar 13			1445.85 35703 x 36251 x 0.2 118.1E+2.4W
2001 Apr 3			1436.07 35783 x 35788 x 0.1 GEO 110.1E
2001 Apr 7			1437.30 35788 x 35832 x 0.0
2001 May 31			1436.19 35774 x 35802 x 0.1 GEO 109.9E
2006 Aug 2			1436.12 35765 x 35808 x 0.0 GEO 109.9E
2010 Apr 28			1436.22 35767 x 35810 x 0.0 GEO 109.8E
2011 Aug 28			1436.48 35765 x 35823 x 0.4 GEO 118.0E

Progress M-04M

 2010-003A

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11F615A60 No. 404, flight 36P.

7288 kg including 880 kg prop and 2685 kg cargo, with 1152 kg BO cargo and 1283 kg OKD liquid cargo plus 250 kg KDU prop usable for ISS orbit correction.

After undocking, it carried out the Otrazhenie-3 experiment.

M04M
Date	Time	Event	Orbit
2010 Feb 3	0345:29	Launch by Soyuz-U	KB LC1
		T+1:58 Blok BVGD sep
		T+2:42 Fairing sep
		T+4:45 Blok A MECO
		T+4:47 Blok A sep
		T+4:57 KhO sep
	0354:16	T+8:46 Blok I MECO
	0354:19	T+8:49 Blok I sep
2010 Feb 3	0734:37	DV1 15.6m/s 40s
	0759:48	DV2 23s 8.8m/s
2010 Feb 4	0449:42	DV3 20s 1.4m/s
2010 Feb 5	0410	At 160m from Zvezda
2010 Feb 5	0425:58	Docked with Zvezda
	0800?	HO
2010 Mar 24	0930	Reboost
2010 Mar 25	0915	Reboost DPO 142 kg 1.0m/s
2010 Apr 23	2030	Reboost 3m/s 20:45
2010 May 10	1115:32	Undocked	91.50 341 x 354 x 51.6
	1118:34	Sep burn 15s
	1506s	burn to lower orbit
2010 May 11			91.43 338 x 351 x 51.6
2010 Jun 9			91.39 335 x 349 x 51.7
2010 Jun 10	0022:00	Orbit raise 9.5s	91.55 347 x 353 x 51.6
2010 Jul 1	0655		91.53 346 x 353 x 51.6
2010 Jul 1	1354:00	Deorbit burn 152s 86.9m/s
	1356:32	Deorbit cutoff
	1432	Reentry
	1440	Debris impact Pacific 37 47S 124 51W

By Invitation Only: A Novel

https://welib.org/md5/2254e2b4f2c58c50c12fc1c0cb9fc3bd

WISE

 2009-071A

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Wide Field IR Survey Explorer, MIDEX spacecraft managed by JPL with Ned Wright (UCLA) as PI. 0.4m telescope. Ball Aerospace RS-300 (NextSat derived)

All sky survey 3.5-23 microns. 500 km SSO day-night terminator.

Launch Nov 2009 by Delta 7320-10

Size 2.9m long 2.0 x 1.7m dia.

Mass 661 kg full 645 kg dry.

Cryo cover is hemisphere 0.5?m dia.

WISE
Date	Time	Event	Orbit
2009 Dec 14	1409:33	Launch by Delta II	V SLC3W
		T+1:04 GEM 1-3 burnout
		T+1:39 GEM 1-3 sep
		T+4:24 MECO
		T+4:38 SEIG-1
		T+4:56 Fairing sep
	1419:56	T+10:23 SECO-1	185 x 554 x 97.50
	1501:13	T+51:40 SEIG-2
	1501:21	T+51:48 SECO-2	522 x 537 x 97.50
	1504:53	T+55:20 Stage 2 separation
	1534:33	T+1:25:00 SES-3 evasive over Arctic
		T+1:25:35 SECO-3	530? x 2110?
	1604:33	T+1:55:00 SES-4 depletion over circa 155W 15S
		T+1:55:46 SECO-4 at 2400 km	2113 x 11086 x 97.5
2009 Dec 29	2230	T+16d Cryostat cover ejection
2010 Jul 17		First sky survey completed
		Half-sky second epoch begun
2010 Aug		Cryogen running out
2010 Sep 29		Cryogen depleted
2010 Oct		Begin NEOWISE warm survey
2011 Feb 17	2000	Hibernation mode, transmitter off
2013 Jan?		Verified healthy in hibernation
2014 Jan		NEOWISE resumes

Payload:

• IR telescope, 40 cm aperture at 12K

• Cryostat 1.9m long 1.2m dia

• 15.7 kg frozen solid H2

• IR instrument (SDL-Utah/UCLA/Wright) with 4 IR detectors: 3.4, 4.6, 12 and 22 micron bands with 47' FOV and 6" (12" at 22 mu) res.

  • 3.4mu and 4.6mu 1024x1024 pixel HgCdTe at 32K

  • 12, 22 mu 1024x1024 pixel SiAs at 8K

High Achiever

 https://www.dewolfemusic.com/search.php?id=28509133&code=4ULYPT

So Not The Drama: A Del Rio Bay Clique Novel

 https://welib.org/md5/3a5053496334921c035b3c2452f1f4c6

Intelsat 11

 2007-044B

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Intelsat Orbital Star 2 platform, 18 Ku and 16 C, for AOR. Originally PAS-11.

Mass 2450 kg launch, 1145 kg dry. Size 4.1 x 3.3 x 2.3m with 22.4m span.

CONUS, Mexico and Latin American DTH and video at 43W.

IS-11 and Optus D2 were launched by L526, V178 Ariane 5GS. IS-11 on a Saab PAS937S adapter and CASA MFD spacer on the Astrium-ST Sylda 5E. Optus D2 on a EADS-CASA 937VB5 adapter on the EPS.

IS-11
Date	Time	Event	Orbit
2007 Oct 5	2202	Launch by Ariane 5GS	CSG ELA3
		T+2:20 EAP sep
		T+3:15 Fairing sep
	2211	T+9:37 EPC MECO	-35 x 1622 x 7.27
	2211	T+9:43 EPC sep
	2211	T+9:50 EPS burn
	2228	T+26:33 EPS MECO 1582 km alt	585 x 35913 x 4.0
	2229	T+27:48 IS-11 sep
	2232	T+30:25 Sylda 5 sep
	2234	T+32:01 Optus D2 sep
2007 Oct 5			638.85 592 x 35793 x 4.0
	2328	Aestus second burn test
2007 Oct 7			702.77 3283 x 35787 x 2.7
2007 Oct 10			1261.26 27892 x 35789 x 0.2
2007 Oct 12	1212	LAM	1433.90 35698 x 35788 x 0.0 GEO 48.2W+0.55E/d
2007 Oct 17		mv in at 47.5W for tests
2007 Oct 30		mv out
2007 Nov 5		mv in at 43W	1436.03 35783 x 35787 x 0.1 GEO 43.2W
2007 Dec 8			1436.12 35780 x 35793 x 0.1 GEO 43.2W
2008 Feb 17			1436.14 35776 x 35798 x 0.0 GEO 43.1W
2010 Apr 29			1436.12 35774 x 35799 x 0.0 GEO 43.0W