JCSAT-5

 1997-075A

---

Japan Satellite Systems' JCSAT 5 (JCSAT 1B) is an HS-601, to be at 150E. Launch by Ariane in Dec 1997. JCSAT 5 was launched atop the Cyclade adapter covering the Equator-S science satellite. Provide communication services for Japan and the Asia-Pacific region.

Mass is 2982 kg launch, 1819 kg BOL, 1308 kg dry. Size is 3.80 x 2.80 x 4.30 m with 26.2 m span.

Info on LAM burns provided by Jun Takei of the JCSAT control center in Yokohama.

In 2005 JCSAT 5/1B had thruster problems which pushed its pointing off-target, and it was replaced by JCSAT 4.

JCSAT 5
Date	Time	Event	Orbit
1997 Dec 2	2252	Launch by Ariane 44P	CSG
	2255	T+3:35 Stage 2 burn
	2256	T+4:38 Fairing 01 sep
	2257	T+5:49 Stage 3 burn
	2310	T+18:51 Stage 3 cutoff
	2312	T+20:59 JCSAT 5 sep
1997 Dec 4			630.68 214 x 35751 x 4.0
1997 Dec 4	0114:38	LAM 1 2279s
1997 Dec 5	0115:14	LAM 2 2656s
1997 Dec 7	0120:28	LAM 3 1945s
1997 Dec 7	0252:54	LAM 4 54s
1997 Dec 7	1431.79 35622 x 35781 x 0.1 GEO 138.3E+1.0E
1997 Dec 8	0045:25	LAM 5 86s
1997 Dec 9			1436.86 35756 x 35808 x 0.1 GEO 139.4E
1998 Jan 3			1436.28 35784 x 35795 x 0.1 GEO 139.4E
1998 Jan		At 150E replace JCSAT 4
1998 Jan 21		mv in	1436.15 35782 x 35793 x 0.0 GEO 150.0E
1998 Feb 2			1436.12 35784 x 35790 x 0.0 GEO 150.0E
1999 Oct 15			1436.12 35780 x 35793 x 0.0 GEO 150.0E
2005 Jan 17		Thruster anomaly, off line for a few days
2005 Jul		Thruster problem recurs
2006 Feb 3			1436.12 35783 x 35790 x 0.0 GEO 149.9E
2006 Feb 5		Move out of GEO
2006 Mar 1		Move in at 128E
2006 Aug 3			1436.18 35784 x 35792 x 0.0 GEO 128.0E

Arabsat 4A

 2006-006A

---

EADS Astrium Eurostar 2000+ satellite; 4B to follow. Launch by ILS Proton 535-11/Briz M 88515 Comms payload by Alcatel. Also called BADR-ONE.

Briz-M failed in transfer orbit; MES-2 ended 3min10s early. Planned duration was 21 min. Since the satellite contract was for on-orbit delivery, the satellite was presumably owned by Astrium in orbit. After the failure, a European insurance group took ownership (J. Oberg, http://www.nbcnews.com/id/11999597/ns/technologyandscience-space/t/arabsat-bites-dust-dashing-hopes)

Mass 3341 kg full 1520 dry 2.5 x 1.8 x 2.9m with 7.5 x 32.0 x 4.5m deployed.

A4A
Date	Time	Event	Orbit
2006 Feb 28	2010:00	Launch by Proton
		T+2:03 St 1 sep
		T+5:32 St 2 sep
		T+5:43 GO sep
		T+9:34 St 3 MECO
	2019	T+9:46 St 3 sep
	2021	T+11:20 MES-1
	2024	T+14:45 Briz-M MECO-1	173 x 173
	2115:23	T+1:05:23 Briz-M MES-2
	2142:54	MECO-2 premature at 27:31
	2146s	T+1:36:14s MECO-2
	2150?	Sep
2006 Mar 1			505 x 14695 x 51.52
2006 Mar 10			503 x 14687 x 51.5
2006 Mar 23			492 x 14688 x 51.6

The High School Journal: December 2007-January 2008

 https://welib.org/md5/75c1d8ad2dc753be8de98c3ca1558dca

Aviation Week: February 11,2008

 https://welib.org/md5/7e99fe39ca39a8579e9b4e9853b4da1e

Friends 4Ever? #7 (Disney High School Musical; Stories from East High)

 https://welib.org/md5/f0acb4f767513acd38a9984096780256

Yubileyniy

 2008-025A

---

NPO PM satellite modified to carry RS-30 amateur radio payload to commemorate the 50th anniversary of Sputnik. Launched with three Gonets-class satellites given Kosmos designations (Kosmos 2437-39).

Yubileyniy
Date	Time	Event	Orbit
2008 May 23	1520:09	Launch by Rokot/Briz-KM	PL LC133/3
		T+2:15? St 1 MECO
		T+2:16? St 1 sep
		T+2:19? St 2 MES
		T+3:04? GO sep
		T+4:58? St 2 MECO
		T+5:18? St 2 VECO
		T+5:19? St 2 sep	-4000? x 200? x
	1525	T+5:25? Briz RB DU-1 2.405 km/s
	1534:10	RB DU-1 MECO	100? x 1511? x 82.5
	1634:25	Briz MES-2, 343 m/s
	1635:22	Briz MECO-2
	1704:18	3 Gonets sats sep	1478 x 1511 x 82.5
	1705:08	RS sep from Briz
	1715:15	Briz depletion 83m/s
	1716:55	Briz depletion MECO	1195 x 1506 x 82.5

Celebrity Style Guide : Teen People

https://welib.org/md5/0256552439ad2b8311430f830ce61d87

People: November 26,2007

 https://welib.org/md5/7c2424926e19ad28c612a7d5e156844b

People: May 12,2008

 https://welib.org/md5/ebf8ca076c4814fbfca1a71f3b730a97

The Penguin Concise Guide to Opera

 https://welib.org/md5/1d57dc22da841ad4173a3d08faa50647

Soyuz TMA-11 (Agate)

 2007-045A

---

No 221, launch by Soyuz FG No 020 on ISS flight 15S.

Crew are Yuriy Malenchenko (Soyuz commander), Peggy Whitson (ISS commander) and Sheikh Muszaphar Shukor Al Masrie (EP-13 crew).

On the way down, Whitson and Malenchenko were joined by Yi Soyeon of South Korea. The PAO failed to separate at the correct time, the spacecraft tumbled and was exposed to strong heating. The resulting ballistic reentry led to a landing 475 km short of the target.

Planned landing was at 50 57 N 67 10 E, actual landing was at 50 31 N 61 07E, 278 km E of Aktyubinsk.  

Mass 7220 kg, of which 1309 kg in BO and 2859 kg in SA. Prop is 879 kg.

Soyuz TMA-11
Date	Time	Event	Orbit
2007 Oct 10	1322:39	Launch by Soyuz-FG No 020	KB LC1
	1331:27	Blok-I sep	194 x 234 x 51.6
2007 Oct 10	1711:07	DV1 SKD 19.2m/s
	1755:40	DV2 10.1m/s
	2046		253 x 258 x 51.6
2007 Oct 11	1428:27	SKD burn 0.8m/s
2007 Oct 12	0730		254 x 259 x 51.6
	1433	At 400m
	1442	Auto mode
2007 Oct 12	1450:05	Docked with Zarya nadir
	1622	HO
2008 Apr 19	0243	HC
	0506:30	Undocked from Zarya
	0510	Sep burn
	0740:46	Deorbit 4:18
	0744	Deorbit cutoff
	0804:37s	Modules sep failed
	0806	Entry
	0807?	Modules sep  - 60 to 66 km
	0815?	Parachutes open
	0829?	Landing
	0908	Helicopter has capsule in sight

SAR-Lupe 4

 2008-014A

---

SAR-Lupe 4
Date	Time	Event	Orbit
2008 Mar 27	1715:27	Launch by Kosmos-3M	PL LC132/1
	1717	Stage 1 sep
	1717	Stage 2 burn
	1723?	Stage 2 MECO
	1735?	Stage 2 burn 2
	1743	Stage 2 sep	94.40 470 x 508 x 98.2

February 18,2006

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

People: March 3,2008

 https://welib.org/md5/f18f55ff712ff2b3d70292a32b4f1f45

Navstar 48

 2008-012A

---

IIR-19 (IIRM-6). SVN 48, PRN 7. Mass 2059 kg.

GPS 48
Date	Time	Event	Orbit
2008 Mar 15	0610	Launch by Delta 7925	CC SLC17A
		T+1:03 SRM 1-6 off
		T+1:05 SRM 7-9 on
		T+1:07 SRM 1-6 sep
		T+2:08 SRM 7-9 off
		T+2:11 SRM 7-9 sep
		T+2:20 Stage 1 dogleg 20s
		T+4:23 MECO
		T+4:31 St 1 sep
		T+4:36 SEIG-1
		T+4:43 St 2 dogleg, 10s
		T+4:57 Fairing sep
	0620	T+10:48 SECO-1	174 x 205 x 37.5
	0712	T+1:02:29 SEIG-2
	0713	T+1:03:12 SECO-2	191 x 1241 x 37.95
	0714	T+1:04:01 spinup
	0714	T+1:04:04 St 2 sep
	0714	T+1:04:42 TES
	0716	T+1:06:08 TECO	193 x 20368 x 40.0
	0718	T+1:08:02 St 3 sep
	0718	T+1:08:04 Yo weight from St 3
		T+1:46:40 SES-3 depletion
2008 Mar 16			355.72 177 x 20327 x 40.1
2008 Mar 17	0921	AKM	20134 x 20152 x 55.1

November 15,2004

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

February 13,2001

 https://web.archive.org/web/20080504032241/http://digest-archive.degrassi.ca/DD125.htm

Us Weekly: December 24,2007

 https://welib.org/md5/ccc59e9dccc36c98c8a6a294dc75ce7f

August 8,2004

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

Apollo: The Definitive Sourcebook

 https://welib.org/md5/7dc9f4878e06855ea54de796e2da5ba3