Spot 2

 1990-005A

---

The second SPOT used the SPOT Mk 1 bus, and was launched on 1990 Jan 22 on an Ariane into an 800 km orbit. The orbit was raised to 825 km by Jan 30 and the satellite was declared operational and turned over to the Spot Image operating team on Mar 23. In addition to the CCD imagers, SPOT 2 carried the DORIS experiment to allow accurate orbit determination.

In Jul 1997 a collision avoidance burn was made to avoid a 400m flyby of object 5061, increasing orbital height by 400m for a day.

SPOT 2
Date	Time	Event	Orbit
1990 Jan 22	0135:27	Launch by Ariane (V35)	CSG ELA2
		T+2:38 St 1 sep
		T+2:40 St 2 MES
		T+3:50 Fairing
		T+4:48 St 2 sep
		T+4:53 St 3 MES
	0152:11	T+16:44 St 3 MECO
	0152:33	T+17:06 SPOT 2 sep
	0155:33	T+20:06 UOSAT D/E sep
	0156:28	T+21:01 Microsat A-D sep
	0159:58	T+24:31 evasion maneuver
			100.78 786 x 805 x 98.7
1990 Jan 23			100.90 800 x 805 x 98.7
1990 Jan 30		At operational orbit
1990 Mar 23		To Spot Image, operational
1993 Sep			101.41 825 x 825 x 98.7
1997 Jul 23	2000:30	Avoidance burn (Object 5061 COLA)
1997 Jul 23	2051:08	Avoidance burn part 2
1997 Jul 24	1815	Return burn
2006 Aug 4			101.41 824 x 826 x 98.7

AMC-10

 2004-003A

---

SES Americom satellite using A2100 bus for digital cable delivery. Launch mass 2315 kg, 907 kg dry.

The satellite would replace Satcom C-4 at 135W. AMC-7 at 137W served as an in-orbit backup.

The launch used a new profile, in which the second Centaur burn, carried out at the equator, lowered inclination to only 12 degrees, decreasing the amount of fuel needed for the satellite's apogee burn.

AMC 10
Date	Time	Event	Orbit
2004 Feb 5	2346:02	Launch by Atlas IIAS AC-165	CC SLC36A
		T+00:59 SRB 3-4 on
		T+01:07 SRB 1-2 off
		T+01:57 SRB 3-4 sep
		T+2:43 BECO
		T+2:46 Booster sep
		T+3:25 Fairing sep
		RL10 nozzles extend
		T+4:30 132 km 3.575km/s	-5600? x 160?
		T+5:00 SECO
		T+5:25 MES1
		T+6:00 169 km, 4.112 km/s
	2355	T+9:38 MECO1	185 x 185
2004 Feb 6	0009	T+23:56 MES2 1:57
	0011s	T+25:53 MECO2
	0014:14	T+28:13 Centaur sep	630.12 210 x 35727 x 12.4
2004 Feb 7		LAM-1	679.11 2698 x 35730 x 9.1
2004 Feb 8		LAM-2	755.02 6468 x 35707 x 6.16
2004 Feb 8		LAM-3	858.21 11363 x 35710 x 4.0
2004 Feb 11?		LAM-4
2004 Feb 12			1431.40 35661 x 35727 x 0.1
2004 Feb 16			1436.15 35775 x 35799 x 0.1 GEO 146.0W
2004 Mar 7			1436.06 35773 x 35797 x 0.0 GEO 146.0W
2004 Apr		Move to 135W
2004 May 10			1436.11 35779 x 35794 x 0.1 GEO 135.0W
2006 Aug 8			1436.10 35778 x 357904 x 0.1 GEO 135.0W

DirecTV 2

 1994-047A

---

GM Hughes Electronics DirecTV Inc.'s second satellite was launched in Aug 1994. DBS 2 is also known as DirecTV 2.

DBS 2
Date	Time	Event	Orbit
1994 Aug 3	2357	Launch by Atlas IIA	CC LC36A
1994 Aug 4	0001	Atlas sep
	0001	Centaur MES-1
	0007	Centaur MECO-1
	0021?	Centaur MES-2
	0022	TLE perigee
	0022?	Centaur MECO-2
	0024?	Centaur sep
1994 Aug 3			704.14 206 x 39473 x 26.9
1994 Aug 6	0500?	LAM-1
1994 Aug 6			759.71 2943 x 39459 x 18.0
1994 Aug 7	0700?	LAM-2
1994 Aug 8			1048.23 16218 x 39389 x 5.1
1994 Aug 8	1730?	LAM-3
1994 Aug 8			1455.40 32837 x 39489 x 0.1 (?)
1994 Aug 9			1429.53 31845 x 39470 x 0.0 GEO 82.8W+1.6E
1994 Aug 10			1531.24 35782 x 39475 x 0.0 DSO 76.8W+22.4W
1994 Aug 12			1436.49 35514 x 36074 x 0.1 GEO 100.5W+0.1W
1994 Sep 3			1436.09 35775 x 35797 x 0.0 GEO 103.0W
1994 Oct 10		mv to 100.7W
1994 Oct 28			1436.08 35773 x 35798 x 0.0 GEO 100.7W
1995 Jul 25			1436.10 35777 x 35796 x 0.0 GEO 100.8W
1999 Oct 19			1436.10 35776 x 35796 x 0.0 GEO 100.7W
2006 Jan 18			143.10 35776 x 35797 x 0.0 GEO 100.7W
2006 Feb		Sold to Telesat, renamed Nimiq 4i
2006 Feb		move in 91W
2006 Aug 3			1436.10 35773 x 35800 x 0.1 GEO 91.1W

STS-92 (Discovery)

 2000-062A

---

Discovery remained in the VAB until Atlantis launched because of concerns about having two stacks on the pads during hurricane season.

Launch mass was 115125 kg. Landing mass was 92739 kg (press kit values). Mass at docking is 111023 kg. At Oct 16, docked mass is 171784 kg. ISS mass is 69445 kg? STS mass is 102339 kg? At Oct 21 mass is 97911 kg.

Cargo transfer of 9978 kg including 8324 kg Z1 and 1156 kg PMA-3, 498 kg other. That 498 kg includes internal cargo transfer; it may also include the ETSDs (188 kg?) and the DDCUs (116 kg), or these may be included in the Z1 mass. For the time being I will assume it is internal cargo. SODB says deployed is 9978, retrieved 133. Non-deployed bay cargo of 2122 kg includes the 300? kg ICBC, the 1400 kg pallet, about 160 kg of DDCU carriers, and 262 kg remaining - which may be extra pallet-attached hardware.

The SGANT deployed is 374 kg per a prelaunch (DAC9) analysis. I have 88 kg for antenna, 34 kg for SGTRC, leaving 252 kg for the boom and attach hardware. The total of Z1 ORUs is then 2267 kg; if Z1 is 8324 kg total, then it is 6057 bare. Another source gave 8765 kg for Z1 mass which would require the other figures to be adjusted accordingly.

On Oct 5, a concern about the ET explosive bolts caused a scrub. Weather forbade on Oct 9 attempt. On Oct 10 a small loose pin lying on the ET noticed by the ice team caused a scrub.

The Ku-band system failed, taking out live TV and requiring the crew to use the TCS laser rangefinders and optical star trackers for navigation during rendezvous.

On Oct 14, a power spike took out the keel camera and the SVS during RMS uncradle, but backup systems restored the SVS.

In the first EVA, the Z1-to-Unity umbilicals are connected. The SASA (S-band) is moved from the DDCU install location to a deployed location. The SGANT (Ku-band) is moved to a new location on Z1 and deployed.

On EVA-4, Wisoff and Lopez-Alegria finished up the work. They cycled the Z1/P6 latch, deploy an ammonia coolant attachment panel, and move the Z1 keel pin to a storage location. They then tested the SAFER backpacks, making semi-free flights with a slack tether.

After two waveoffs, landing was at RW22 EAFB for the first Edwards landing in 4 years.

STS-92
Date	Time	Event	Orbit
2000 May		SRB stacking
2000 Aug 21		Tow from OPF/1 to OPF/3
2000 Aug 24		Tow to VAB/3
2000 Aug 25		Mate to ET/SRB
2000 Sep 11		Rollout to LC39A
2000 Oct 5		Scrub T-10?hr
2000 Oct 9		Scrub WX T-10?h
2000 Oct 10		Scrub T-20min
2000 Oct 11	2317:00	Launch	KSC LC39A
	2319:03	SRB sep
	2319:13	OMS Assist
	2319:54	OMS Ass CO
	2325:26	MECO	74 x 323 x 51.6
	2325:46	ET sep
2000 Oct 12	0000:32	OMS-2 53.6s 24.9m/s	89.31 158 x 322 x 51.6
	0001:27	OMS-2 CO
	0054	PLBD open
	0235:58	OMS-3 NC1 31s 14m/s	89.80 179 x 349 x 51.6
	0236:30	OMS-3 CO
	1517s	RMS uncradle
	1639:55	NC2 27s 2m/s	89.80 180 x 349 x 51.6
	1800?	RMS berth
	2353:52	OMS-4 NC3 139s 46.6m/s	91.41 311 x 375 x 51.58
	2355:31	OMS-4 CO
2000 Oct 13	1228:55	OMS-5 NC4 33s 15.4m/s
	1229:27	OMS-5 CO
	1311:17	RCS NCC 0.4m/s
	1409:00	OMS-6 L TI burn 16s 4.0m/s	92.12 375 x 381 x 51.6
	1409:17	OMS-6 CO
	1428	MC1
	1505	MC2
	1522	MC3
	1539s	At -Rbar 180m
	1604s	At +Rbar 75m
	1616s	Skeep at 52m on +Rbar
	1715	Resume approach
	1745:10	Docking with PMA-2
	1757:55	Hard dock
	2030	PMA-2 entry
	2115	Unity entry
2000 Oct 14	1250?	RMS uncradle
2000 Oct 14	1257	Power spike
	1557:14	Z1 grapple
	1615	Z1 unberth from PLB
	1820	Z1 dock to Unity
	1840	Z1 install complete
	1905:30	RMS ungrapple
	1910	Z1 attachment complete
		RMS ungrapple
2000 Oct 15		EVA-1 McArthur, Chiao
	1406	RMS uncradle
	1411	Begin depress
	1425:39	Depress
	1425?	HO
	1427	Battery power
	1430	TC open
	1446	McArthur egress
	1450	McArthur on RMS, to Unity, get APFR
	1455?	Chiao egress
	1600	Connect Z1 cables
	1610	Relocate SASA-1, unbolt from Z1
	1627	SASA-1 reinstalled
	1800	Remove Ku dish.
	1846	Deploy Ku band Space-to-Ground (SGANT) antenna
	1930	ETSD-1 off PLT
	1940	Install port ETSD box from PLT to Z1
	2040?	Ingress
	2050?	HC
	2054:42	Repress begins 6:28 (NASA)
2000 Oct 16		EVA-2 Wisoff, Lopez-Alegria	92.10 374 x 381 x 51.6
	1345	RMS powerup
	1355	Begin depress
	1357	Hold depress for leak
	1400	Resume depress
	1403	At 5 psi
	1407	Resume depress
	1412:07	Depress
	1412?	HO
	1414	TC already open
	1415	Battery power
	1421	Wisoff (Safer-3) egress
	1429	Lopez-Alegria egress
	1543:30	RMS grapple PMA-3
	1556	Unbolting PMA-3
	1602	PMA-3 unlatch from SLP
	1614	PMA-3 unberth
	1705	PMA-3 near CBM
	1735	PMA-3 soft dock
	1740	PMA-3 capture
	1743	PMA-3 bolted to Unity
	1759:35	RMS ungrapple PMA-3
	2030?	Lopez ingress
	2103	Reboost-1 30:34 2m/s
	2109	Wisoff ingress
	2110	Close TC
	2115	HC
	2121:30	Repress: 7:07 (NASA)
	2133	End reboost
2000 Oct 17	EVA-3 Chiao, McArthur	92.16 379 x 381 x 51.6
	1414	EVA-3 depress begin
	1427:01	EVA-3 depress complete?
	1428?	HO
	1430	EVA-3 on battery
	1433	TC open
	1439	McArthur egress (SAFER 4)
	1446	Chiao egress (SAFER 3)
	1451	Depress valve cap released
	1606	port DDCU unberthed
	1615	Install DDCU-HP 4B
	1648	Installed DDCU-HP 3B
		Z1 umbilicals attach
	1750	ETSD unberthed
	1800	ETSD install
		Transfer tool bag to ETSD
	1930	Z1 Keel pin moved
	2015	Z1 Keel pin relocated
	2113	Ingress
	2114	HC
	2117:28	Repress 6:48 (NASA)
	2245:59	Reboost-2 32:20 2m/s
	2318	Reboost stop
2000 Oct 18	0000		92.22 381 x 385 x 51.6
		EVA-4 Wisoff, Lopez-Alegria
	1443	Begin depress
	1448	5 psi hold
	1450?	Depress complete
	1458:03	Depress (MR)
	1458?	HO
	1500	Battery power
	1507	TC open
	1507	Egress
	1530	Z1 claw latch tested
		Z1 FRGF grapple fixture relocated on Z1
		Z1 truss tray deployed
	1850	Setup for SAFER
	1855	Wisoff semi-free SAFER test from FGB to bay
	1939	Wisoff end SAFER flight, 46min or less
	1949	Lopez-Alegria semi-free SAFER test
	2016	L-A end SAFER flight, 27min
	2145	Ingress
	2146	TC closed?
	2149	HC
	2156:32	Repress 6:56 (NASA)
	2223	Reboost-3 29:32 2m/s
	2253	Reboost stop
2000 Oct 19	1400	Enter Unity and Zarya	92.28 381 x 391 x 51.6
2000 Oct 20
	1317s	Hatches closed to ISS	92.27 381 x 390 x 51.6
	1427s	Reboost
	1508:21	Undocking
	1518	At 45mm begin half loop
	1531	RCS burn 0.6m/s
	1552:59	RCS burn, sep 15s 1.2m/s	92.24 379 x 389 x 51.6
2000 Oct 22	1457	PLBD closed
	1637	DO cancelled, PLBD open
2000 Oct 23	1815	PLBD closed
	2143	DO cancelled, PLBD open
2000 Oct 24	1701	PLBD closed
	1952:00	OMS DO 3:06 104.1m/s	92.24 378 x 389 x 51.6
	1955:04	OMS CO	39 x 387 x 51.6
	2028:17	Entry interface 124 km
	2033	At 50 km
	2059:41	MGTD EAFB RW22
	2059:54	NGTD
	2100:49	WS
2000 Nov 1		Mate to SCA
2000 Nov 2	1651	Depart EAFB on SCA
	2000	Arrive Altus AFB, OK
		Arrive Whiteman AFB, Missouri
2000 Nov 3	1823	Depart Whiteman
	1910	Arrive Robins AFB, GA
	2135	KSC SLF
2000 Nov 4	0330	Tow to OPF/1

GOES 5

 1981-049A

---

Geostationary Operational Environmental Satellite 05 (GOES E) was launched by Delta 3914 from Cape Canaveral LC17A at 2229 on 1981 May 22. At 2252 the Star 37E third stage left GOES 5 in a 192 x 49768 km x 26.6 deg transfer orbit. The next day the TE-M-616 apogee motor circularized the orbit to 33840 x 49667 km x 0 deg. GOES 5 reached geostationary orbit at 85 deg W on Jun 5 for checkout, and was then moved to the GOES E position, replacing SMS 2 on Aug 5. The VAS failed on 1984 Jul 29 but GOES 5 was kept at the GOES E position for data relay work with the DCS.

GOES 5
Date	Time	Event	Orbit
1981 May 22	2229	Launch by Delta 3914	CC LC17A
		T+0:57 SRM 1-5 off
		T+1:04 SRM 1-5 sep
		T+1:04 SRM 6-9 on
		T+2:01 SRM 6-9 sep
		T+3:44 MECO
		T+3:52 Stage 1 sep
		T+3:58 SES-1 4:20
		Fairing
	2237	T+8:18 SECO-1	88.10 157 x 204 x 28.73
	2249	T+20:14 SES-2 51s
	2250	T+21:05 SECO-2	163 x 2618 x 28.1
	2251	T+22:07 spinup
	2251	T+22:09 St 2 sep	186? x 2350? x 28.1
	2251	T+22:49 TES
	2252	T+23:33 TECO
	2253	T+24:42 Star 37E sep	921.04 192 x 49767 x 26.6
1981 May 23	0700?	Apo 1 over 53E
1981 May 24	1255?	Star 27 burn 35s, eq crossing
	1300?	Star 27 eject
1981 May 24			1751.49 33840 x 49667 x 0.5
1981 May 25			1742.79 33731 x 49456 x 0.5
1981 May 29			1619.82 33800 x 44820 x 0.5 GEO 62.6E+40.9W
1981 Jun 1			1539.53 35457 x 40118 x 0.5 GEO 36.3W+24.26W
1981 Jun 2		In geo region	1458.81 35450 x 37009 x 0.5 GEO 76.9W+5.6W
1981 Jun 3			1430.09 35451 x 35886 x 0.5 GEO 87.8W+1.5E
1981 Jun 5		mv in	1436.12 35714 x 35859 x 0.5 GEO 84.8W
1981 Jun 5			85W
1981 Jun 30			1436.27 35713 x 35866 x 0.4 GEO 85.5W
1981 Jul 24		mv out	1436.33 35737 x 35844 x 0.4 GEO 86.7W+0.07W
1981 Aug 5			75W
1981 Aug 24			1435.89 35771 x 35793 x 0.3 GEO 75.5W+0.05E
1981 Oct 3			1436.08 35774 x 35797 x 0.2 GEO 74.4W
1982 Jan			75W
1983 Jan 2			1435.96 35782 x 35785 x 0.3 GEO 74.6W
1984 Jul 29		VAS failed
1984 Aug		Data relay for GOES 6
1986 Jan 4			1435.72 35766 x 35792 x 0.0 GEO 74.3W
1987 Feb 28			1436.03 35779 x 35790 x 0.4 GEO 74.7W
1987 Mar 13		mv out	1436.57 35781 x 35810 x 0.4 GEO 75.3W+0.13W
1987 May 14		mv in	1436.29 35784 x 35796 x 0.5 GEO 105.9W+0.06W
1987 May 30			1436.18 35782 x 35794 x 0.6 GEO 106.3W
1988 Jan 13			1436.07 35780 x 35791 x 1.2 GEO 108.2W
1988 Jan 29		mv out	1437.14 35789 x 35824 x 1.2 GEO 108.4W+0.3W
1988 Mar 29			1432.29 35695 x 35728 x 1.4 GEO 59.8W+0.9E
1988 Apr 6		mv in	1436.13 35766 x 35808 x 1.4 GEO 64.2W
1988 Jun 16			1436.37 35778 x 35805 x 1.6 GEO 66.3W
1989 Jan 6			1436.24 35712 x 35866 x 2.1 GEO 65.0W
1989 Apr		Begin drift
1989 May 10			1436.38 35781 x 35802 x 2.5 GEO 66.2W+0.08W
1989 May 31			1436.74 35730 x 35868 x 2.7 GEO 68.8W+0.16W
1989 Aug 7		mv in	1436.28 35780 x 35799 x 2.7 GEO 64.5W
1989 Sep 21			1436.07 35767 x 35804 x 2.8 GEO 64.0W
1989 Nov 15		last mv	1436.36 35782 x 35800 x 2.9 GEO 65.6W+0.07W
1989 Dec 25			1436.20 35742 x 35834 x 3.0 GEO 65.8W+0.03W
1990 Jul 18		Deactivated
1990 Sep			1436.99 35798 x 35812 x 3.6 GEO 92.7W+0.2W

Adapting the Arthurian Legends for Children: Essays on Arthurian Juvenilia

https://welib.org/md5/b6afc13edddd398150afea25f8f7b873

USA-111

 1995-027A

---

The UHF F/O F5 (EHF F5) satellite was launched by AC-116 on 1995 May 31. It was the second Block II satellite with an EHF payload.

UHF F5
Date	Time	Event	Orbit
1995 May 31	1527.01	Launch by Atlas Centaur	CC LC36A
	1529.46	BECO
	1529.49	Booster sep
	1530.36	Fairing sep
	1531.40	SECO
	1531.42	Atlas sep
	1532.04	Centaur MES1
	1538.52	Centaur MECO1
	1549.56	Centaur MES2
	1551.20	Centaur MECO2
	1554.52	Centaur sep	317 x 26628 x 27.0
1995 May 31			461.58 289 x 26522 x 27.0
1995 Jun		LAM-1	289 x 36500?
1995 Jun		LAM-2
1995 Jun 4			810.00 8300 x 36511 x 13.4
1995 Jun 4	2230?	LAM-3
1995 Jun 5			1189.16 25090 x 36515 x 6.5
1995 Jun 6	1400?	LAM-4
1995 Jun 6			1401.57 33697 x 36518 x 5.2
1995 Jun 7	1340?	LAM-5
1995 Jun 7			1437.20 35096 x 36520 x 5.1 GEO 172.1W+0.15E
1995 Jun 11			1436.31 35061 x 36519 x 5.1 GEO 169.6W+0.06W
1995 Jul 1			1436.29 35060 x 36520 x 5.1 GEO 172.9W+0.06W
1995 Jul 11		mv out
1995 Oct 23			1436.08 35770 x 35802 x 5.0 GEO 71.8E
1996 Jan 6			1436.03 35778 x 35792 x 4.8 GEO 72.4E
1999 Jul 9			1436.10 35766 x 35807 x 3.4 GEO 72.2E
2000 Oct		Move to 100W
2001 Mar 16			1436.21 35784 x 35794 x 2.9 GEO 100.7W
2005 Mar 6			1436.12 35752 x 35821 x 2.0 GEO 100.5W

Yaogan 1

 2006-015A

---

SAST Remote Sensing (Yaogan) satellite, mass 2700 kg. Thought to be a radar satellite. Also called Yaogan Weixing, YW-1.

Yaogan
Date	Time	Event	Orbit
2006 Apr 26	2248	Launch by CZ-4C	TY
	2250	T+2:32? St 1 sep
	2250	St 2 burn
	2250	T+2:47? Fairing sep
	2254	T+6:48? Stage 2 MECO
	2254	T+6:49? St 2 sep
		Stage 3 burn 1
	2258?	Stage 3 MECO 1
	2300?	Stage 3 sep	601 x 621 x 97.8
		Stage 3 MES-2 depletion
		Stage 3 MECO-2	452 x 624 x 97.8
2006 Apr 29			97.03 606 x 626 x 97.8
		Orbit raise	97.21 623 x 626 x 97.8
2006 May 10			97.28 628 x 629 x 97.8

The Clique

 https://welib.org/md5/c72c6f2e7048fe62738c30de363672a2

TD-1A

  1972-014A

---

The TD-1A satellite was ESRO's first astronomy satellite, the TD standing for Thor Delta (the launch vehicle). It was built by Matra and controlled from the ESOC facility, TD-1A made the first ultraviolet stellar sky survey. The early loss of the satellite’s tape recorders meant that extra tracking stations were pressed into service.

TD-1A
Date	Time	Event	Orbit
1972 Mar 12	0155:08	Launch by Delta N	V
		SRM sep
	0158:45	T+3:37 MECO
		T+3:39 St 1 sep
	0158:48	T+3:40 SES-1 6:21
		T+3:56 Fairing sep
	0205:03	T+9:55 SECO-1
	0245:36	T+50:28 SES-2
	0245:40	T+50:32 SECO-2
	0247	T+52:07 Delta sep	95.4 524 x 551 x 97.6
1972 Mar 15		1-m optics cover ejected
1972 Apr 19		No.2 tape recorder problem
1972 May 23		No.1 tape recorder failed
1973 Oct		S59 and S2/68 switched off; S77 on
1973 Dec		S2/68 back on for airglow
1974 May 5		end of stabilization
1975?		end of transmissions
1980 Jan 9		Reentered

International Reference Guide to Space Launch Systems

https://welib.org/md5/311482cc6e9678bbc038791fba99af5c

The Perfect Manhattan

https://welib.org/md5/80f1e14af28837008e8016064bb3b2d9

TDRS-3

 1988-091B

---

The TDRS C payload was named TDRS 3 on reaching orbit. TDRS 3 was carried into space on the first `return to flight' mission, STS-26R. Discovery was launched on 1988 Sep 29 and the TDRS/IUS was deployed at The first IUS burn, at 2250 on Sep 29, left TDRS in a 632.98 min, 287 x 35797 km x 26.71 deg orbit. The second burn, at 0406 on Sep 30, put it in a 1433.48 min, 35673 x 35798 km x 2.3 deg circular orbit. By Oct 5 it had reached the TDRS WEST position at 171 W. In around 1992 it was moved to 62W as TDRS SPARE, but in 1994 it was reassigned to move back to the TDRS WEST position.

TDRS 3
Date	Time	Event	Orbit
1988 Sep 29	1537:00	Launch from LC39B
	1539:05	SRB sep, 46.3 km
	1545:33	MECO, 110.0 km	88.03 65 x 289 x 28.5 (PK)
	1545:50	ET sep, 111.9 km	88.21 69 x 302 x 28.5 (OMS dV)
	1616:56	OMS-2 (2:21) 68m/s	90.55 299 x 304 x 28.5
	1619:18	OMS-2 CO
	2100?		90.55 300 x 303 x 28.5
	2150:04	TDRS deploy
1988 Sep 29	2250:04	IUS-7 SRM-1
	2252:33	SRM-1 burnout
	2257:33	RCS-1
	2257:53	RCS-1 end
1988 Sep 29			632.98 287 x 35797 x 26.7
1988 Sep 30	0356:49s	SRM-2 exit cone deploy
1988 Sep 30	0402:29s	SRM-1 sep
1988 Sep 30	0406:48	IUS SRM-2 1:49
	0408:37	IUS SRM-2 burnout
	0412:18?	RCS-2 burn 1:37
	0413:55?	RCS-2 burn end
	0421?	TDRS solar array deploy
	0444:50s	SRM-2 sep
	0450?	IUS SRM-2 CAM burn
	0451?	IUS SRM-2 RCS depletion burn
1988 Sep 30			1433.48 35673 x 35798 x 2.3
1988 Sep 30			1434.75 35718 x 35803 x 0.1
1988 Oct 1			1435.07 35722 x 35811 x 0.1 GEO 178.1W+0.25E/d
1988 Oct 4			1424.40 35554 x 35561 x 0.1 GEO 172.3W+3E/d
1988 Oct 18		mv in	1436.50 35785 x 35803 x 0.0 GEO 149.5W
1988 Nov 29			1436.11 35772 x 35801 x 0.0 GEO 151.1W
1988 Dec 13			1436.01 35769 x 35801 x 0.1 GEO 151.0W
1988 Dec 21		mv out
1989 Jan 16		mv in	1436.23 35776 x 35801 x 0.2 GEO 171.1W
1989 Jan		TDRS W	171W
1990 Apr 16			1436.02 35777 x 37593 x 0.1 GEO 171.0W
1990 May 2		Drift to 174W
1990 May 16			1436.16 35774 x 35801 x 0.0 GEO 174.1W
1991 Jan 27			1436.07 35777 x 35794 x 0.7 GEO 174.4W
1991 Oct 7			1436.02 35565 x 36005 x 0.0 GEO 173.9W
1991 Oct 8		mv out
1991 Nov 3			1424.64 35555 x 35568 x 0.1 GEO 99.7W+2.9E
1991 Dec 10		mv in	1436.01 35771 x 35798 x 0.1 GEO 62.2W
1992 Jan		TDRS SPARE	62W
1992 May 10			1436.13 35776 x 35797 x 0.5 GEO 61.9W
1993 Aug 4			1436.21 35774 x 35803 x 0.3 GEO 61.9W
1994 May 16			1436.00 35777 x 35792 x 1.0 GEO 61.8W
1994 May 22		mv out
1994 Jul 13			1442.44 35899 x 35921 x 1.1 GEO 153.7W+1.5W
1994 Jul 30		mv in TDRS W	1436.18 35779 x 35797 x 1.1 GEO 171.3W
1995 Mar 29			1435.95 35772 x 35795 x 1.6 GEO 171.0W
1995 Apr 22		mv out
1995 May 29		mv in	1436.21 35768 x 35809 x 1.7 GEO 85.2E
1998 Mar 8			1436.01 35770 x 35799 x 3.7 GEO 85.0E
1999 Jun 13			1436.11 35771 x 35802 x 4.6 GEO 85.4E
2003 Sep 5			1436.23 35779 x 35799 x 7.6 GEO 84.5E
2006 Jul 23			1436.12 35710 x 35863 x 9.7 GEO 85.1E