Ranger 7

  1964-041A

---

Ranger VII (Ranger B, P-54) was launched at 1650:07 on 1964 Jul 28 by Atlas Agena B from Cape Canaveral. The Atlas separated at 1655:15, Agena burn 1 was from 1655:56 to 1658:34 placing the probe in a 188 x 192 km x 28 deg parking orbit. Agena reignited at 1718:32 until 1720:01 and separated at 1722, making an avoidance maneuver at 1729. Ranger VII made a midcourse correction at 1027:09 on 1964 Jul 29. The flight gave NASA and JPL a badly needed success. The first photos were sent back at 1306 on Jul 31, and continued up to impact at 1325:49 on 1964 Jul 31 in a lunar mare region later renamed Mare Cognitum (the Known Sea) in honor of the flight. Location was 10.7S 20.7W.

Ranger 7
Date	Time	Event	Orbit
1964 Jul 28	1650:07	Launch by Atlas LV-3A/ Agena B	CKAFS LC12
	1652:23	BECO
	1652:26	Booster sep
	1655:13	Fairing
	1655:15	Atlas 250D sep
	1655:56	Agena 6009 MES-1
	1658:34	Agena MECO-1	182 x 203 x 28.83
	1718:32	Agena MES-2
	1720:01	Agena MECO-2
	1722:36	Agena sep	185 x 526173 x 29.0
	1729:06	Agena avoidance, retro burn
1964 Jul 29	1027:09	MCC 49s 29.9m/s
	1027:59	MCC off	-35 x 475454 x 28.7
1964 Jul 31	1306	First photos
1964 Jul 31	1325:49	Impact
1964 Jul 31	1630?	Agena flyby 4170km

Georgia Irvin's Guide To Schools: Metropolitan Washington, Independent And Public / Pre-K Through 12

 https://welib.org/md5/9e862e28830e3fe8e9b04196fd306d97

The Complete Wedding Planner

https://welib.org/md5/39bfd474cdb5c94dc369b33654c08aba

Generation Deluxe

https://welib.org/md5/311159dd573f3130d8c632732af73ac7

SSETI Express

 2005-043E

---

The SSETI (Student Space Education and Technology Initiative) Express satellite, a precursor to ESEO, mass 62 kg 0.6 x 0.6 x 0.7m box with 2 panels 1.8m span, to launch to 686 x 686 x 98.3 SSO on Cosmos DMC-3. Carries 10N N2 orbit adjust thruster. Control from Aalborg.

Kosmos
Date	Time	Event	Orbit
2005 Oct 27	0652:26	Launch by Kosmos-3M No 104	PL LC132/1
		T+2:11 St 1 sep
		T+2:26 GO sep
	0700:04	T+7:38 St 2 MECO-1
	0726:40	T+34:14 St 2 MES-2
	0726:53	T+34:27 St 2 MECO-2
	0727:18	T+34:52 Topsat sep
	0727:20	T+34:54 China-DMC sep
	0727:21	T+34:55 Sinah sep
	0727:23	T+34:57 SSETI sep
	0727:24	T+34:58 Mozhaets sep
	0830?	IWE-1 sep
	0832	NCUBE-2 sep
	0837:26	XI-V separation

Payload:

• Langmuir probe

• Earth imager WAC (Wide Angle Camera) and NAC (Narrow Angle Camera)

Molniya 201

  1971-100A

---

The first Molniya-2 satellite was launched in Nov 1971 by 8K78M Molniya from Plesetsk.

Molniya-2 F1
Date	Time	Event	Orbit
1971 Nov 24	0930:02	Launch by 8K78M	PL
		BVGD sep
		GO sep
		T+4:46 Blok A sep
		T+4:56 KhO sep
		T+8:46 Blok-I MECO
	0938	T+8:50 Blok-I sep
		T+53:16 BOZ burn
	1023	T+53:56 BOZ sep
		ML burn
		T+56:46 ML MECO
	1026	T+56:54 ML sep
			712.00 516 x 39552 x 65.5
1971 Dec 10			705.73 462 x 39296 x 65.5
1971 Dec 13			705.91 447 x 39320 x 65.5
1972 Jan 11			705.86 464 x 39301 x 65.4
		Orbit raise
1972 Jan 27			717.72 481 x 39870 x 65.5
1972 Feb 26			717.80 507 x 39848 x 65.5
1972 Oct 24		End of ops
1972 Oct 26			717.55 525 x 39818 x 65.5
1973 Aug 8			717.64 262 x 40085 x 65.5
1973 Oct 2			716.33 180 x 40102 x 65.5
1974 Mar?		Reentered

Palapa B4

 1992-027A

---

Indonesia's Telkom (formerly Perumtel) launched the final Palapa B satellite, Palapa B4, in May 1992.

Palapa B4
Date	Time	Event	Orbit
1992 May 14	0040	Launch by Delta	CC LC17B
		97.5 deg az
		T+1:03 SRM 1-6 off
		T+2:09 SRM 7-9 off
		T+4:20 MECO
		T+4:37 SES-1
		T+4:38 Fairing sep
	0049	T+9:45? SECO-1	185 x 185 x 28.5?
	0101?	T+21:40? SES-2
	0101?	SECO-2	185 x 2800? x 27.5?
	0156?	T+1:16:48 SES-3
	0156?	SECO-3	500? x 2800? x 25.2?
	0157?	St 2 sep
	0158?	T+1:18:28 TES 1:27
	0159?	TECO
	0201?	PAM-D sep	702.97 2806 x 36814 x 22.6
	0204?	Delta evasive burn
	0300?	St 2 perigee
	0400?	St 2 apogee
	0400?	Delta depletion burn	501 x 2791 x 19.7
1992 May 15			702.01 2764 x 36809 x 22.5
1992 May 17	1744?	Star 30BP burn
1992 May 17			1441.72 34952 x 36840 x 0.3 GEO 94.7E+1.4W
1992 May 22		mv in	1436.04 35771 x 35799 x 0.2 GEO 118.0E
1992 May 27			1436.03 35773 x 35797 x 0.03 GEO 118.02E+0.01/d
1995 May 7			1436.14 35785 x 35790 x 0.0 GEO 118.1E
1999 Jun 14			1436.09 35778 x 35794 x 0.0 GEO 118.0E
2005 Aug 16			1436.17 35784 x 35791 x 0.6 GEO 117.5E

Progress M-48

 2003-039A

---

Launch mass was 7283 kg; mass at docking was 6934 kg. It carried 2566 kg of cargo, including 879 kg of prop, 420 kg of water. Last minute payloads including the GCF crystal sample experiment for the CGBA, bungee cords for the treadmill, and shoes, as well as a satellite phone and GPS locator for use in case of an off-course reentry, as well as 4 NGL laptops, personal effects and hardware for Expedition 8, and ESA experiments for Pedro Duque's mission.

 

Progress M-48
Date	Time	Event	Orbit
2003 Aug 29	0147:59	Launch by Soyuz-U	KB
		T+1:58 BVGD sep
		T+2:41 GO sep
		T+4:47 Blok A sep
		T+4:57 KhO sep
		T+8:45 MECO
		T+8:49 Blok I sep
	0524	DV1
	0602	DV2
2003 Aug 30	0239	DV3a
	0323	DV3b
	0446 TORU test
2003 Aug 31	0151s	DV4
	0234s	DV5, range 80 km
		Flyaround at 400m
		Stationkeeping at 170m
	0330	Final approach
	0340:45	Docked with Zvezda
2004 Jan 28	0835:56	Undocked
	0839:00	DV 15s DPO sep burn
	1311:00	Deorbit 182s 94.36 m/s
	1346:03	Entry
	1351:10	Breakup, 70 km
	1357:12	Debris impact 3500 km E NZ

NATO 3D

 1984-115A

---

NATO IIID was launched in Nov 1984. Unlike the earlier satellites in the series, it used a Thiokol Star 27 apogee motor.

NATO IIID
Date	Time	Event	Orbit
1984 Nov 14	0034:01	Launch by Delta 3914	CC LC17
		T+1:04 SRM 1-5 sep
		T+1:04 SRM 6-9 on
		T+2:01 SRM 6-9 sep
		T+3:48 MECO
		T+3:56 St 1 sep
		T+3:58 SES-1 Stage 2 burn 4:20
		T+4:05 Fairing sep
	0042:19	T+8:18 SECO-1	166 x 680?
	0054:15	T+20:14 SES-2 51s
	0055:06	T+21:05 SECO-2	680 x 2310 x 21.5
		T+22:07 Spinup
	0056:11	T+22:10? Stage 2 sep
	0056:41	T+22:40 Stage 3 burn 44s
	0057:25	T+23:24 TECO
	0058	T+24:30? Stage 3 sep
1984 Nov 14			647.30 409 x 36409 x 22.9
1984 Nov 16	0205	Star 27 burn 35s
1984 Nov 16			1428.08 35256 x 36002 x 6.0 GEO 143.3E+2.0E
1984 Nov 19		Drift mv
1984 Nov 20			1416.37 35187 x 35611 x 6.0 GEO 163.1E+5.0E
1984 Dec 5			1416.27 35185 x 35609 x 6.0 GEO 117.8E+5.1E
1984 Dec 12			1426.11 35571 x 35610 x 5.9 GEO 127.9W+2.5E
1985 Jan 20			1426.22 35573 x 35612 x 5.9 GEO 30.6W+2.5E
1985 Jan 21		Braking
1985 Jan 25		mv in	1436.11 35785 x 35788 x 5.8 GEO 29.8W
1985 Feb 27			1436.15 35782 x 35792 x 5.8 GEO 29.9W
1985 Mar 18			1436.59 35789 x 35803 x 5.7 GEO 50.3W+0.1W
1985 Mar 24			1435.78 35773 x 35787 x 5.7 GEO 50.7W
1985 Apr 21			1436.15 35783 x 35791 x 5.7 GEO 49.8W
1986 Oct 4			1435.91 35780 x 35785 x 4.4 GEO 49.8W+0.04E
1986 Oct?		Move to 21W
1987 Jan 5			1436.20 35778 x 35798 x 4.1 GEO 21.3W
1987 Nov 5			1436.23 35781 x 35796 x 3.4 GEO 21.7W
1988 Aug 28			1435.94 35777 x 35789 x 2.6 GEO 21.7W
1989 Apr 2			1436.07 35780 x 35791 x 2.0 GEO 20.8W
1990 Feb 24			1436.11 35771 x 35802 x 1.3 GEO 20.6W
1990 Sep 29			1436.24 35783 x 35795 x 0.8 GEO 21.8W+0.04W
1991 Jan 7			1436.18 35781 x 35794 x 0.6 GEO 20.4W
1991 Jan 28		mv out
1991 Apr 13		mv in	1436.06 35776 x 35794 x 0.5 GEO 30.1W
1992 Jan 1			1436.15 35781 x 35794 x 0.6 GEO 29.4W
1993 Jan 29			1436.14 35782 x 35792 x 1.5 GEO 30.9W
1993 Jun 12			1436.16 35779 x 35796 x 1.8 GEO 30.9W
1993 Jun 28		mv out
1993 Aug 4		Mv in	GEO 22W
1993 Aug 15			1436.11 35783 x 35790 x 1.9 GEO 21.0W
1995 Aug 14			1436.11 35777 x 35796 x 3.4 GEO 21.1W
1997 Feb 26			1435.84 35779 x 35791 x 4.4 GEO 21.1W
1997 Mar			GEO 21W
1997 Mar		Relocate	GEO 18.5W
1997 Mar 26			1435.70 35777 x 35779 x 4.4 GEO 18.5W
1999 Apr 13		mv out	1436.32 35781 x 35800 x 5.7 GEO 18.4W+0.06W
1999 Apr 28			GEO 19.5W
2000 Jun 10			GEO 19.8W
2003 Feb 6			1436.15 35783 x 35791 x 5.2 GEO 19.4W

Bergdorf Blondes: A Novel

 https://welib.org/md5/cedc907b86f2f814333424e309ff9bd6

Navstar 27

 1992-058A

---

Navstar SVN 27 was launched on 1992 Sep 9 and placed in plane F-1. The second stage was put in a low inclination 19.8 deg post-depletion orbit. Working backwards from the stage 3 orbit and making the parking orbit pass over Cape Canaveral, it seems that the parking orbit inclination may have been changed to 34 deg for a launch azimuth of 110 deg.

Navstar 27
Date	Time	Event	Orbit
1992 Sep 9	0857:00	Launch by Delta 7925	CC LC17A
		SRM 1-9 sep
		St 1 sep
	0901	T+4:40? SES-1
	0908	T+11:00? SECO-1	185 x 185 x 34
		T+20? SES-2 36s?
	0917	T+20? SECO-2	180? x 724? x 34.0?
	0918	T+21? St 2 sep
	0919	T+22? TES 1:24
	0920	T+23? TECO
	0922	T+25? St 3 sep	356.91 183 x 20394 x 34.75
	0955?	SES-3 depletion
		SECO-3	98.59 658 x 724 x 19.8
1992 Sep 11	0608?	Star 37XFP burn
1992 Sep 14			722.96 19979 x 20630 x 54.8
1992 Sep 30		In service
1997 Feb 1		Operating at slot F-1
2000 Jul		Operating at A-4
2005 Aug 10		Decommissioned

The Real Space Cowboys

https://welib.org/md5/55a4cbc6f0b9f431263e2063f480b076

American dream : the houses at Sagaponac

 https://welib.org/md5/185b27a3c3bed4b8ad3fa9b9536ec882

Creating the International Space Station

 https://welib.org/md5/6f08c7e33e5cfd06fed433e26665180c

ATS 3

  1967-111A

---

Applications Technology Satellite 3 followed on the successful ATS B mission and was, if possible, even more successful, operating into the 1980s. It carried both communications and weather experiments.

Launch was at 2337 UT on 1967 Nov 5 from pad 12 at Cape Kennedy. The SR-28-3 kick motor fired at 1532 UT on Nov 6, and ATS III reached a 35791 x 36130 km x 0.5 deg orbit on station at 47 W within the day. In 1970 the meteorological imaging camera was handed over to NOAA for operational use. There was an antenna malfunction in Jul 1971.

ATS 3 was drifting back and forth between 46W and 100W from 1968 to 1970 when it was stationed at 63W and then (in Nov 1970) at 46W. From 1971 to 1976 ATS 3 remained at 69W. In early 1977 it arrived at 105W, where it remained until 2000, after officially completing its mission in 1978.

ATS 3
Date	Time	Event	Orbit
1967 Nov 5	2337:00	Launch by Atlas Agena D
		T+2:08 BECO
		T+2:11 Booster sep
		T+4:49 SECO
		T+5:09 VECO
		T+5:13 Atlas 5103 sep	-4110 x 180 x 28.33
		T+6:12 Agena 6153 MES-1
		T+6:21 Fairing sep
	2345:53	T+8:53 Agena MECO-1, 12 min coast	184 x 192 x 28.4
1967 Nov 6	0002:05	T+25:05 Agena MES-2
	0002	Perigee from TLEs
1967 Nov 6	0003:23	T+26:23 Agena MECO-2
1967 Nov 6	0006	T+29:08 Agena sep	627.87 177 x 35643 x 28.4
1967 Nov 6	1532	AKM burn
1967 Nov 7	2329		1436.47 35772 x 35815 x 0.4 GEO 48.0W+0.1E
1967 Nov 20		Drifting	GEO 49.4W+2.2E
1967 Nov		Initial location at 52.3W
1967 Dec		Relocated to 95W
1968 Mar 9			GEO 86.5W
1968 Oct 21			x 0.7 46.4W
1968 Dec 5			x 0.7 47.2W+0.5 W/d
1969 Jan 25			GEO 72.4W
1969 Feb 15			x 0.5 73.2W+0.5 E/d
1969 May 16			GEO 73.3W
1969 Jun 25			x 0.2 52.1W+0.8 E/d
1969 Jul 2			GEO 46.9W+0.11W
1969 Aug 25			x 0.1 47.8W
1969 Oct 13			x 0.2 45.7W+0.1 E/d
1970 Apr 1			GEO 80W+0.1W
1970 Jun 13			x 0.8 67.9W+0.1 E/d
1970 Aug 14			GEO 63.3W+0.0E
1970 Oct			x 1.1 63.5W
1970 Nov			GEO 46W
1971 Jan			x 1.3 65.6W
1971 Apr 3			x 1.5 80.0W
1971 May 31			1436.15 35665 x 35910 x 1.7 GEO 79.0W+).02E
1971 Jun 10			x 1.7 79.1W
1971 Sep 16			x 2.0 69.4W
1971 Dec 21			x 2.2 69.0W
1972 Mar 15			x 2.4 69.7W
1973 Jun 21			x 3.6 69.6W
1973 Dec 28			x 4.0 69.4W
1974 May 3			x 4.3 69.7W
1974 Sep 15			x 4.6 68.8W
1975 Jan 12			x 4.9 69.5W
1975 Sep 13			x 5.4 69.7W
1976 May 26			x 5.9 70.1W
1976 Dec 7			x 6.3 84.4W
1977 Mar 18			1436.99 35715 x 35892 x 6.5 GEO 105.3W+0.2E
1977 Mar 24			1436.14 35717 x 35857 x 6.5 GEO 105.1W+0.0E
1978 Nov 15			105.3W
1980 Sep			105W
1982 Oct			105W
1983 Oct 31			105.3W
1985 Aug			105.2W
1985 Sep			105.2W
1998 May 5			1436.08 35719 x 35853 x 14.8 GEO 105.5W+0.00E
2003 Feb 8			1436.09 35718 x 35854 x 13.0 GEO 105.9W+0.00W

FSW-22

 2005-033A

---

FSW 22
Date	Time	Event	Orbit
2005 Aug 29	0845?	Launch by CZ-2D
	0855?	Stage 2 sep
			89.52 203 x 297 x 63.0
2005 Aug 30	0829	Orbit raise	204 x 322 x 63.0
2005 Sep 13			203 x 321 x 63.0
2005 Sep 16	0303?	Deorbit 58E 61N
	0328	RV landed after 16.9d
2005 Sep 16	0546		202 x 321 x 63.0
2005 Oct 1			195 x 274 x 63.0

Space Shuttle Columbia: Her Missions and Crews

 https://welib.org/md5/c87e1667e5075d1900d7389cfc67da3c

Kosmos 2417

 2005-050A

---

Kosmos-2417
Date	Time	Event	Orbit
2005 Dec 25	0507:10?	Launch by Proton-K 410-12	KB LC81-23
		T+2:06 St 1 sep
		T+3:17 GO sep
	0512	T+5:38 St 2 sep
	0516	T+9:40 St 3 MECO
	0516	T+9:52 St 3 sep
	0556?	T+49:19? DM 11S861 No. 106L burn 1
	0502?	T+55:06? DM MECO 1
	0836?	DM MES2
	0838	DM MECO 2
	0838	DM sep	19134 x 19143 x 64.9

Himawari 5

 1995-011B

---

The GMS-5 (Himawari-5) satellite was launched on 1995 Mar 17 on the third H-II flight. This flight used extra SSB (Solid Sub Boosters) in addition to the SRBs.

GMS 5
Date	Time	Event	Orbit
1995 Mar 18	0801	Launch by H-II	TNSC
		T+1:16 SSB burnout 25 km 1.3 km/s
		T+1:30 SSB sep 36 km 1.6 km/s
		T+1:34 SRB burnout
		T+1:37 SRB sep 42 km 1.6 km/s
		T+3:39 Upper fairing sep 128 km 2.8 km/s
		T+5:47 MECO
		T+5:56 Stage 1 sep 222 km 5.3 km/s
		T+6:02 Stage 2 SES-1	-4400 x 250 ?
	0813	T+12:20 SECO-1
	0814	T+13:16 SFU separation
	0817	T+16:11 Lower fairing sep
	0826	T+25:03 SES-2
	0828	T+27:02 SECO-2
	0828	T+27:52 Stage 2 sep from GMS
			647.17 346 x 36465 x 25.1
1995 Mar 19	0056	Star 27 burn
	0110	Star 27 sep
			1419.06 35483 x 36321 x 1.1 GEO 151.7E+4.3E
1995 Apr 1			1434.74 35730 x 35789 x 1.1 GEO 159.6E+0.3E
1995 Apr 14			1436.08 35783 x 35789 x 1.0 GEO 159.7E
1995 Jun 5			1436.11 35784 x 35789 x 0.9 GEO 159.7E
1995 Jun		Move to 140E
1995 Jun 13		Begin data
1995 Jun 26			1436.10 35779 x 35793 x 0.9 GEO 140.1E
1996 Oct 26			1436.15 35784 x 35790 x 0.4 GEO 140.0E
1999 Oct 6			1436.26 35427 x 36151 x 0.4 GEO 140.1E
2001 Jul		S Hemisphere coverage reduced
2005 May 5			1436.20 35780 x 35796 x 3.8 GEO 140.1E

Progress M-47

 2003-006A

---

Launch 1259:40 UTC. Progress 247 on mission 10P.

Mass 7230 kg. 880 kg of prop, 1328 kg of dry cargo. (NK: 7267 kg). Mass at undocking was 7356 kg.

On Feb 11 it reboosted the station's orbit following the loss of Columbia. Operator error resulted in an underburn and an altitude raise of only 7 instead of 10 km.

Progress 247
Date	Time	Event	Orbit
2003 Feb 2	1259:40	Launch by Soyuz-U E15000-680	KB
		T+1:58 Block BVGD sep
		T+2:41 GO sep
		T+4:47 Block A sep
		T+4:57 KhO sep
	1308:25	T+8:45 St 3 MECO
	1308:29	T+8:49 St 3 sep
2003 Feb 4	1305	Zvezda Kurs activated
	1438	Zvezda arrays feathered
	1449	Docked with Zvezda
	1915s	HO
2003 Feb 11	1050	TCM 4.2 m/s 1200s
2003 Mar 12	2258	DPO test burn 1.3m/s raise perigee 4 km
2003 Mar 13	2337s	DPO test burn 0.3m/s
2003 Apr 4	1259	ISS reboost 1.8m/s 3.1 km 179 kg
2003 Apr 10	1055	ISS reboost 1.5m/s 2km 140 kg
2003 Aug 27	2248:08	Undock
2003 Aug 28	0155	Deorbit 190.9s 103.9m/s
	0228	Entry over Pacific
	0238	Impact near 40 39S 133 46W

Movie star homes : the famous to the forgotten

 https://welib.org/md5/517eba24062ff1f6df1677797e7dbfcf

Asiasat 3

 1997-086A

---

Asia Satellite Telecommunications' HS-601HP Asiasat 3, was to provide Asia-wide C-band coverage and 3 high power Ku band beams. Total power is 9.9 kW. Launched by Proton in Dec 1997, it was stranded in transfer orbit when the second DM3 burn failed, shutting down after only 1s of the 110s burn. Mass was 3480 kg launch, 2560 kg BOL, 1822? kg dry. Size 4m high, 3.1m wide, 26.2m span.

Asiasat 3 was to have replaced Asiasat 1 at 105.5E, with the latter satellite moving to 122E.

In mid 1998 a remarkable rescue strategy evolved: a lunar gravity assist. Asiasat 3 became the property of Hughes Global Services (HGS) in Apr 1998 and was informally renamed HGS-1. The apogee was raised in stages until a TLI burn in May placed it on a free-return lunar flyby trajectory.

In Apr 1999 HGS-1 was purchased by PanAmSat and renamed PAS 22.

Asiasat 3
Date	Time	Event	Orbit
1997 Dec 24	2319	Launch by Proton 394-01/DM3-6L	KB
	2321	Stage 1 sep T+2:07
	2324	Stage 2 sep T+5:35
	2324	Fairing sep T+5:44
	2324	8S812 burn T+5:40
		8S812 shutdown T+9:38
	2328	8S812 sep T+9:49	180 x 210? x 51.6
	2329	T+10:44 PB (perekhodnikiy blok) sep
1997 Dec 25	0036	DM3 burn 1
1997 Dec 25	0036	Eq crossing at 10W
	0037	DM3 MECO-1
1997 Dec 25	0537	DM-3 burn 2 T+6:18
	0537	DM-3 burn 2 failed after 1s
		10 DM3 debris objects tracked
	0540?	DM3 sep
1997 Dec 27			638.25 365 x 35989 x 51.05
1998 Jan 5			638.31 375 x 35982 x 51.1
1998 Feb 8			638.29 393 x 35963 x 51.1
1998 Apr 1?		Renamed HGS-1
1998 Apr 7			638.33 412 x 35947 x 51.24
1998 Apr 9		LAM-1 burn	638.59 417 x 35955 x 51.2
1998 Apr 13		LAM burn	638.51 392 x 35977 x 51.3
1998 Apr 14		LAM burn	1244.05 402 x 63475 x 51.3
1998 Apr 15		LAM burn	1512.05 397 x 74124 x 51.3
1998 Apr 16		LAM burn	1882.60 399 x 87854 x 51.35
1998 Apr 18	0726	LAM-7?	2479.12 425 x 108172 x 51.2
1998 Apr 21	1423	LAM-8?	2492.67 447 x 108592 x 51.2
1998 Apr 23	1214	LAM-9?	3800.17 432 x 148144 x 51.21
1998 Apr 26		LAM-10?	6078.06 365 x 207527 x 51.5
1998 Apr 30		LAM-11?	240 x 319786 x 52.1
1998 May 8	0042	LAM-12 TLI 2min	344 x 413596 x 52.2
1998 May 13	1852	LOS
	1920	AOS
	1955	Lunar flyby 1, 6250 km
			42061 x 475000? x 18
1998 May 17	0300s	Perigee 42061 km?
1998 May 17	0308	Burn	35646 x 475763 x 18.2
1998 May 25	0300	Apogee	488000 km
1998 Jun 2			37451 x 474241 x 18.3
1998 Jun 2	0240	Perigee, Trim burn 30min
1998 Jun 6	1630s	Lunar flyby 2 , 34300 km
1998 Jun 11		Trim burn
1998 Jun 14	1615	Perigee, Trim burn 46min
	1750	Trim burn 2min	2777.10 35883 x 82253 x 8.9
1998 Jun 16	1429	GEO insertion	1679.89 35869 x 44996 x 8.8
1998 Jun 17	1829	GEO insertion 12min
1998 Jun 18			1433.92 35622 x 35865 x 8.7 GEO 152.5W+0.5E
1998 Jun 19			35681 x 35963 x 8.7 GEO 152W+0.5/d
1998 Aug 10			1436.05 35676 x 35895 x 8.6 GEO 153.6W
1998 Sep 28		mv out	1435.60 35652 x 35900 x 8.5 GEO 150.5W+0.1E
1998 Nov 16			1436.50 35649 x 35939 x 8.4 GEO 153.9W
1999 Apr		GEO dr
1999 Apr		To Panamsat as PAS 22
1999 May 25			1436.00 35601 x 35968 x 8.0 GEO 60.4W
1999 Oct 15			1436.12 35587 x 35986 x 7.8 GEO 59.5W
2002 Jul 1		60W mv out