Something I might work on later,who knows?

 That's Terri MacGregor-Jeremiah behind the desk,she's my assistant and kinda my gal pal too. Her fiancé (yes,she's already taken his surname) is Craig Jeremiah,one of the new teachers at the high school.

Hey,Cameron,I see you're filming,eh?

You're on candid camera,Ter! Mind being interviewed?

No,I don't. Lemme just.....okay,I'm ready.

So,what's your full name,anyway? I've always wanted to know.

Theresa Claire MacGregor-Jeremiah.

How about some basic facts about yourself? Nice skirt-thing,by the way.

Thanks,I got it on layaway at Clifton Park Center! I graduated from Green High in 2010.....you were class of '16,right?

Indeed.

I'm originally from Carmelide, moved here in 1997 with my family. My parents are Todd and Bethany MacGregor: they manage a chain of farms and farming-related businesses across the Northeast and Maritime States and are worth about $450,000. I have one older sister, Olivia, who graduated from GHS in 2005. I played JV and varsity soccer and varsity tennis in high school and I got to be prom queen in 2009 alongside Gavin Mason as king.

What about college?

I did three years at D'Youville in Buffalo,and I returned here in early 2015.

And Craig,what about him? I remember he went to school here.

Yep,he was class of '09. We started dating late in my senior year here.

Artemis

 2001-029A

---

The second ESA heavy communications technology satellite was the SAT-2/DM Advanced Relay Technology Mission (Artemis) was built by Alenia Spazio for ESA using the Italsat bus. Originally scheduled for launch in 1996  [693], the DRS precursor technology mission was delayed until 2000 and oriented to mobile and inter-satellite communications. In 1996 it was moved from Ariane 5 to the Japanese H-IIA, but was later moved back again after H-II delays. Mass is 3105 kg full. Size is 4.8h 8.0wide (with antennas) and 25m span.

4.86 x 2.85 x 2.95m, span 24.73m.

Artemis was placed above SYLDA, which contained BSAT-2B.

Artemis together with Inmarsat 3 AOR and IOR provides the EGNOS European GPS augmentation. It opeated as an IOR-W (Congo) satellite.

The S400 LAE will perform GEO insertion; relocation will be done by the set of 10N RCS biprop thrusters attached to the S400. Biprop load is 1538 kg. Ion propulsion will be used for NSSK. Artemis carries two DASA RIT-10 thrusters and two MMS EIT T5 thrusters with 40 kg of Xe. Isp is 3000s and thrust is 20mN. Deduced dry mass is 1527 kg.

The EPS stage only got to 80 percent of planned thrust and cutoff 1min 20sec early, because of a combustion instability in the Aestus engine. Designers annouced that mixing the propellant more slowly would fix the problem.

Artemis was later raised to a 30900 x 30940 km orbit, significantly below geosynchronous, and then finally by Feb 2003 to GEO.

Avanti bought the satellite in 2014 and in 2016 relocated it to 123E under a contract from the Indonesian ministry of defence, preserving Indonesia's rights to the old Garuda-1.

Artemis
Date	Time	Event	Orbit
2001 Jul 12	2158:00	Launch by Ariane 5G	CSG ELA3
		T+0:07 Liftoff
		T+2:24 EAP sep
		T+3:25 Fairing sep
	2207:59	T+9:59 EPC cutoff
	2208:06	T+10:06 EPC sep
	2208:28	T+10:28 EPS burn
	2208:31	T+10:31 Aestus problem, 80 percent thrust
	2223:28	T+25:28 Aestus cutoff early
		T+26:48 Aestus cutoff due
	2226	T+28:06 Artemis sep
	2228	T+29:58 Sylda 5 sep
	2233	T+35:35 BSAT-2b sep
2001 Jul 14			318.48 592 x 17548 x 2.9
2001 Jul 18	1519	Perigee burn 1	345.35 609 x 19245 x 3.0
2001 Jul 19		Perigee burn 2
2001 Jul 19		Perigee burn 3
2001 Jul 20		Perigee burn 4
2001 Jul 20		Perigee burn 5
2001 Jul 21	1432		546.86 660 x 30886 x 2.9
2001 Jul 22		Apogee burn 1
2001 Jul 22	1211		579.84 2446 x 30864 x 2.2
2001 Jul 23		Apogee burn 2
2001 Jul 24		Apogee burn 3, parking orbit
2001 Jul 27	1553		1195.43 30902 x 30964 x 0.8
2001 Aug 12			1195.18 30897 x 30958 x 0.8
2001 Dec 4			1194.85 30901 x 30941 x 0.8
2002 Feb 20		Ion thruster burns resume
2002 Feb 21			1195.50 30921 x 30948 x 1.0
2002 Mar 31			1206.45 31118 x 31205 x 1.0
2002 Apr 24			1222.75 31415 x 31583 x 1.0
2002 Jul 18			1284.11 32678 x 32833 x 1.1
2002 Aug 30			1312.77 33289 x 33384 x 1.2
2002 Sep 27			1330.09 33628 x 33741 x 1.2
2002 Oct 27			1353.26 34073 x 34225 x 1.3
2002 Nov 26			1378.52 34589 x 34714 x 1.4
2002 Dec 5			1386.40 34770 x 34845 x 1.4
2003 Jan 3			1409.15 35224 x 35290 x 1.5
2003 Jan 17			1421.28 35488 x 35504 x 1.5 GEO 7.0W+3.7E
2003 Jan 31			1432.32 35664 x 35760 x 1.6 GEO 21.2E+1.0E
2003 Feb 5			1436.29 35494 x 36086 x 1.5 GEO 21.0E
2006 Aug 1			1436.11 35776 x 35797 x 4.8 GEO 21.4E
2009 Jun 1			1436.08 35772 x 35799 x 7.4 GEO 21.5E
2015 Feb 15		AVANTI takes over operation
2016 Apr 22			1436.06 35773 x 35798 x 12.3 GEO 21.3E
2016 May 20			1436.06 35775 x 35795 x 12.3 GEO 20.7E
2016 May 25		Move out	1434.42 35732 x 35775 x 12.3 GEO 24.2E+0.5E/d
2016 Nov 17		Move in 123E	1436.06 35772 x 35799 x 12.5 GEO 123.0E
2017 Oct 29			1436.17 35776 x 35800 x 12.9 GEO 123.2E

The International Space Station: Operating an Outpost in the New Frontier

 https://welib.org/md5/18fa9cfb0f55f360ca97756b9e68dfc2

Apollo Pilot: The Memoir of Astronaut Donn Eisele

 https://welib.org/md5/33f7704a3bff90fedcc91254b0ae0f66

Echostar 6

 2000-038A

---

Launch mass 3700 kg, 1493 kg dry. Size 5.5h 8.7 antenna span, 30.7 solar array span. Launch by Atlas IIAS AC-161 with 14' PLF from LC36B. Loral FS-1300 satellite. S/C sep T+28:55 to 167 x 38651 x 26.5 deg.

Echostar VI
Date	Time	Event	Orbit
2000 Jul 14	0521:00?	Launch by Atlas IIAS	CC LC36B
		T+0:58 SRB 3-4 burn
		T+1:17 SRB 1-2 sep
		T+1:55 SRB 3-4 sep
		T+2:44 BECO
		T+2:47 Booster sep
		T+3:25 Fairing sep
		T+4:57 SECO
		T+4:59 Atlas sep
		T+5:15 Centaur MES-1 4:30
		T+9:51 Centaur MECO-1	155 x 437 x 28.29
		T+24:42 Centaur MES-2
		T+26:19 Centaur MECO-2
	0549:55?	T+28:55 Centaur sep
2000 Jul 15			673.84 149 x 38015 x 26.6
2000 Jul 15?		LAM-1
2000 Jul 16?		LAM-2
2000 Jul 17?		LAM-2
2000 Jul 17			1445.09 33973 x 37951 x 0.2
2000 Jul 20			1390.81 33873 x 35917 x 0.1
2000 Jul 23			1435.79 35653 x 35907 x 0.1
2000 Jul 27			1436.51 35768 x 35820 x 0.1 GEO 147.9W
2000 Aug 14			1436.01 35759 x 35810 x 0.1 GEO 147.9W
2000 Aug 18		Relocate to 119W
2000 Sep 21			1436.07 35781 x 35790 x 0.1 GEO 118.9W
2003 Jan 23			1436.10 35778 x 35795 x 0.0 GEO 119.1W
2003 Feb 7		Relocating
2003 Feb 19			1436.09 35775 x 35797 x 0.0 GEO 110.1W
2006 Aug 2			1436.09 35771 x 35801 x 0.0 GEO 110.4W
2008 Jun 27			1436.09 35775 x 35797 x 0.09 GEO 110.4W
2008 Jul 7		Move out
2008 Jul 30		Move in at 72.7W
2008 Aug 1			1436.09 35775 x 35795 x 0.03 GEO 72.8W
2010 Jan 31			1436.12 35774 x 35799 x 0.0 GEO 72.7W
2010 Feb 16		Move out
2010 Mar 2		Move in at 62W
2010 Mar 18			1436.11 35778 x 35795 x 0.0 GEO 61.7W
2011 Jan 24			1436.10 35774 x 35799 x 0.1 GEO 61.7W
2011 Feb 6		Move out
2011 Feb 15		Move in at 77W	1436.11 35784 x 35789 x 0.0 GEO 77.0W
2013 Apr 2			1436.10 35773 x 35800 x 1.1 GEO 76.8W
2013 Apr 3		Move out
2013 Apr 15		Move in at 96.2W	1436.09 35772 x 35800 x 1.2 GEO 96.2W
2018 May 7			1436.09 35774 x 35799 x 4.8 GEO 96.3W