Progress M1-2

 2000-021A

---

11F615A55 No 252 was Progress M1-2, launch mass 7280 kg. The vehicle was heavily laden with fuel to raise Mir's orbit. It carried 200 kg of fuel as well as 1939 kg of other cargo.

The vehicle undocked on Oct 15, during the STS-92 mission to ISS.

Progress M1-2
Date	Time	Event	Orbit
2000 Apr 25	2008:02	Launch by Soyuz-U	KB
	2012	Blok A sep
	2016	Blok I MECO
	2016:51	Blok I sep
	2353:17	TCM1
2000 Apr 26	0037:54	TCM2	89.40 235 x 253 x 51.7
2000 Apr 26	2103:55	TCM3 1.1m/s
2000 Apr 27	2128:47	Docked Kvant
2000 Apr 28			91.13 327 x 332 x 51.6
2000 May 2			91.98 358 x 384 x 51.6
2000 May 8			92.07 367 x 384 x 51.6
2000 Oct 15	1809:51	Undocked
	2241:23	Deorbit over Pacific
	2329:40	Reentry

DMSP 15

 1982-118A

---

DMSP satellite 17540 (S-6) was the first of an upgraded series, the Block 5D-2. For this spacecraft, the Thor/Star 37XE launch vehicle was replaced with a refurbished Atlas E ICBM. The 5D-2 retained the integral Star 37S kick stage to circularize the orbit. The first 5D-2, DMSP Block 5D-2 S-6, was launched on 1982 Dec 20 to becom F-6. In addition to the OLS weather imager, F-6 (17540) carried a vertical temperature profile radiometer, and three instruments to study energetic processes in the ionosphere - an electron spectrometer, an X-ray spectrometer and a plasma monitor.

DMSP 17540
Date	Time	Event	Orbit
1982 Dec 21	0238	Launch by Atlas E	V
	0240	T+2:04 Booster sep
	0240	T+2:24 Fairing sep
	0243:21	T+5:21 SECO
	0243:50	Atlas sep
	0248:27	T+10:27 Star 37S burn 43.4s
	0249:10	Star 37S burnout
	0249:43	T+11:43 Orbit trim, 816 x 828
	0255	Solar array deploy
			817 x 839 x 98.7
1983 Jan		OLS covers jettison
1987 Aug 24		OLS failed
1993 Aug		Still transmitting

He’s The One

https://welib.org/md5/051df217a2292ef8fc10c2b70ff90b3b

DFH-7

  1976-117A

---

FSW No. 3 recovered its capsule after 3 days in space,owing to the mission undergoing attitude control problems.

FSW
Date	Time	Event	Orbit
1976 Dec 7	0436	Launch by CZ2	JQ
	0438	T+2:10 MECO
	0438	Stage 2 burn
	0440?	T+4:02? Stage 2 MECO
	0443?	Stage 2 VECO
	0443?	CZ-2C sep	91.0 172 x 479 x 59.5
1976 Dec			90.9 174 x 469 x 59.5
1976 Dec 9	0344?	Capsule sep
	0344?	Retro
1976 Dec 9	0357	Capsule recovered after 3d
1977 Jan 2		Reentered

USA-153

 2000-065A

---

DSCS 3 B11 was launched by Atlas 2A. It was the second with SLEP enhancements and will replace B4. Size is 1.8 x 2.1m with 11.6m span. Launch mass 1230 kg. Control from 3SOPS/Schriever.

DSCS III B-11
Date	Time	Event	Orbit
2000 Oct 20	0040	Launch by Atlas IIA AC-140	CC SLC36A
		T+2:44 BECO
		T+2:47 Booster sep
		T+3:15 71 km 2.86 km/s
		T+3:52 Fairing sep
		T+4:41 SECO
		T+4:44 Atlas sep
		T+5:01 Centaur MES-1
	0050	T+10:09 Centaur MECO-1	148 x 898 x 29.3
		T+22:18 Centaur MES-2
	0103	T+23:44 Centaur MECO-2
	0106	T+26:39 Centaur sep

The Lancelot-Grail Reader: Selections from the Medieval French Arthurian Cycle

 https://welib.org/md5/c37acb9456f54bd3fc2bc8f01c9e28af

Hexagon 10

  1975-051A

---

HEXAGON Mission 10 maintained its orbit until around Oct 27; then dipped the perigee to 148 km, went into an elliptical 175 x 272 km orbit, and finally to a 165 x 240 km orbit before deorbiting on Nov 5.

HEXAGON 10
Date	Time	Event	Orbit
1975 Jun 8	1830	Launch by Titan IIID	V SLC 4E
		T+1:49? Stage 1 burn 2:27
		T+1:55 SRM burnout
		T+1:55 SRM sep
		T+4:16 Stage 1 MECO
		T+4:16 Stage 1 sep
		T+4:16 Stage 2 burn
		T+5:05? Fairing
	1837?	T+7:44? Stage 2 MECO
	1838?	T+8:00 Stage 2 sep
			88.8 154 x 269 x 96.4
1975 Jun 8	2056		88.68 156 x 262 x 96.4
	2300?	Subsat eject?
1975 Jun 10			88.78 155 x 272 x 96.4
1975 Jun 24	2043?		SRV-1 recovered
1975 Jul 1			88.74 156 x 267 x 96.4
1975 Jul 28		Mapping camera op 198 last image
1975 Jul 29		SRV-2 recovered
1975 Jul 29	2114?	SRV-5 deorbit opp
	2150?	SRV 1210-5 recovered after 51d
1975 Jul 29			88.71 154 x 267 x 96.3
1975 Aug 3		DB-12 turned off
1975 Aug 16			88.69 152 x 266 x 96.3
1975 Sep 4	2104?	SRV-3 recovered
1975 Sep 13			88.87 153 x 283 x 96.3
1975 Oct 6	2100?	SRV-4 recovered
1975 Oct 7			88.66 146 x 270 x 96.2
1975 Oct 28			88.32 148 x 234 x 96.2
1975 Oct 30			88.92 175 x 267 x 96.3
1975 Nov 5	1200		88.46 165 x 230 x 96.34
1975 Nov 5	2128?	Reentered after 150d

Symphonie 2

  1975-077A

---

The Symphonie 2 (MV2) satellite built by the CIFAS/Aerospatiale consortium for CNES and DFVLR was launched in Aug 27. It joined MV1 at 11.5W. Space Command elements were not released for much of 1985, but it appears that the orbit was raised to 1440 minutes in the third quarter of that year and the satellite was presumably decommissioned at that time.

Symphonie 2
Date	Time	Event	Orbit
1975 Aug 27	0141:00	Launch by Delta 2914	CC LC17
		T+0:38 SRM 1-6 out
		T+0:39 SRM 7-9 on
		T+1:17 SRM 7-9 out
		T+1:27 SRM 1-9 sep
		T+3:48 MECO
		T+3:56 St 1 sep
	0145:01	T+4:01 Delta SES-1 4:49
		T+4:50 Fairing
	0149:50	T+8:50 SECO-1 169 km 7.955 km/s	170 x 706? x 27.0?
	0205:05	T+24:05 SES-2 17s 137m/s? 372 km
	0205:22	T+24:22 SECO-2	409 x 2019 x 25.3
	0206:16	T+25:16 St 2 sep
	0206:56	T+25:57 TES 44s
	0207:40	T+26:40 TECO
	0208:55	T+27:54 St 3 sep	413 x 37974 x 13.16
		SES-3 experimental, 10s
		SECO-3
1975 Aug 29	1548	LAM burn to GEO, 19:50
	1608	LAM complete
1975 Aug 29?		Despin weights?
1975 Aug 30			1436.1 35768 x 35806 x 0.20 GEO 11.5W
1976 May		Drift off station
1976 Jun		On station	GEO 11.5W
1977 Jan 21			1436.18 35750 x 35826 x 0.5 GEO 11.4W
1979 Sep 30			GEO 11.5W
1980 Aug 19			1436.09 35748 x 35825 x 2.0 GEO 11.3W
1982 Oct			GEO 11W
1984 Jul			GEO 11W
1984 Oct 15			1436.14 35747 x 35827 x 5.3 GEO 11.3W
1985 late		Orbit raise to 1440 minutes
1987 Apr 22			1440.43 35853 x 35889 x 7.5
1994 Mar 2			1440.47 35847 x 35896 x 12.9
1999 Apr 19			1440.57 35853 x 35895 x 14.8

Hexagon 14

 1978-029A

---

Mission 14 operated in a 160 x 240 km orbit from Mar 16 to Apr 22; from Apr 23 to Sep 9 it was in a 160 x 255 km orbit. Its orbit entered a period of rapid decay on Sep 9 and it was deorbited on Sep 11.

HEXAGON 14
Date	Time	Event	Orbit
1978 Mar 16	1840?	Launch by Titan IIID	V SLC4E
		T+1:49? Stage 1 burn 2:27
		T+1:55 SRM burnout
		T+1:55 SRM sep
		T+4:16 Stage 1 MECO
		T+4:16 Stage 1 sep
		T+4:16 Stage 2 burn
		T+5:05? Fairing
	1847?	T+7:44? Stage 2 MECO
	1848?	T+8:00 Stage 2 sep
			88.5 160 x 240 x 96.4
1978 Mar 17		Titan stage 2 reentered	(166 x 231 x 96.4)
			88.47 160 x 237 x 96.4
1978 Mar 17			88.42 157 x 234 x 96.4
1978 Apr 1			88.43 157 x 236 x 96.4
1978 Apr 20	2100?	SRV-1 MAR
1978 Apr 22	0622		88.47 161 x 235 x 96.4
1978 Apr 23	1950?	Orbit raise
1978 Apr 23	2042		88.77 165 x 262 x 96.4
1978 Apr 29			88.60 163 x 247 x 96.4
1978 May 1			88.67 167 x 249 x 96.4
1978 May 16		Map op 253
1978 May 31		Op 300
1978 Jun 1			88.56 164 x 242 x 96.4
1978 Jun 1	2109?	SRV-2 MAR
1978 Jun 12		Op 325
1978 Jun 14		Op 340
1978 Jun 21		Op 360
1978 Jul 1			88.73 165 x 258 x 96.4
1978 Jul 6		Op 380
1978 Jul 10		Op 386
1978 Jul 11	2044?	SRV5 deorbit opp
	2120?	SRV 1214-5 recovered after 117d
1978 Jul 12			88.61 164 x 247 x 96.34
1978 Jul 22	2120?	SRV-3 MAR
1978 Aug 1			88.67 164 x 252 x 96.3
1978 Sep 2			88.63 162 x 250 x 96.3
1978 Sep 9	2039?	SRV-4 deorbit
1978 Sep 9	2308		88.51 164 x 236 x 96.3
1978 Sep 11	1159		88.26 158 x 218 x 96.3
1978 Sep 11	2125?	Reentered after 179d

Kosmos 1215

 1980-083A

---

Kosmos-1215
Date	Time	Event	Orbit
1980 Oct 14	2041	Launch by 11K65M	Plesetsk
	2043	S3 burn
	2049?	T+8m? S3 MECO-1
	2114?	T+33m? S3 MES-2
	2114?	S3 sep
1980 Oct 14			95.1 498x550x74.0
1983 May 12		reentered

STS-86 (Atlantis)

 1997-055A

---

Like earlier Mir flights, STS-86 was flown with the internal airlock present, and the shell of the external airlock in the payload bay supporting the Orbiter Docking System. The internal airlock would be removed during the next maintenance period.

Lawrence was replaced by Wolf on Jul 31 since she was too small (1.60m) to operate the Orlan EVA suit, and NASA wanted the US astronaut available to support Spektr repair EVAs. A GAS payload was removed from the payload bay to save mass in favor of extra replacement parts for Mir. G-036, for El Paso Community College, was on a GABA in bay 13S together with the SEEDS can.

The EVA suits for STS-86 featured the first operational use of SAFER, using the first two production flight units.

The Spektr Solar Array Cap (SSAC), loaded at the last minute, was installed in the airlock until needed for the EVA. The EVA would retrieve the MEEP packages from the SO, and would test the SAFER hand controller. DTO 671 involved tests of the common PFR, and the rigidized MUT (Multi Use Tether) with its end effector and tool carrier. EV1 was Parazynski with PLSS 5, EV2 was Vladimir Titov with PLSS 4 in the first use of a US EVA suit by a Russian.

STS-86
Date	Time	Event	Orbit
1997 Jul 31		ET/SRB mate
1997 Aug 12		OV/ET mate
1997 Aug 18		Roll to LC39A
1997 Sep 26	0234:19	Launch	LC39A
	0236	SRB sep
	0242:49	MECO T+8:30	88.28 81 x 297 x 51.7
	0242	ET sep
	0316:09	OMS 2 108s 52m/s	90.05 256 x 297 x 51.7
	0407:48	PLBD open
	0559:09	NC1 OMS-3 59s 29m/s
	1726:15	NC2 OMS-4 37s 17m/s
1997 Sep 27	0322:20	NC3 RCS 18s 1m/s
	1559:25	NC4 OMS-5 26s 13m/s
	1634:13	NCC RCS 7s 0.5m/s
1997 Sep 27	1731:50	TI burn 23s 2m/s
	1741:13	MC1
	1825:13	MC2
	1842:13	MC3
	1852:13	MC4
	1902	200m on +Rbar
		Rbar approach
	1957:46	Docking
	2006:05	Hard dock
	2145	Hatch open
1997 Sep 28	1549	Wolf to Mir crew, Foale to STS
	1634	Official crew exch. (MR)
1997 Oct 1	1715	Begin depress
	1725?	Depress EVA-1
		Parazynski, Titov
	1729	On battery power
	1732	Complete depress (MR)
	1738	Hatch open, EV1 egress
	1742	EV2 egress
	1828	MEEP 2 retrieved from SO
	1850	MEEP 2 stowed
	1916	MEEP 1 retrieved
	1940	MEEP 1 stowed
	1957	MEEP 4 retrieved
	2015	MEEP 4 stowed
	2030	MEEP 3 retrieved
	2044	MEEP 3 stowed
	2103	SSAC transferred to SO
	2125	SAFER tests
	2223	Ingress
	2230	Repress
1997 Oct 2	2245	Hatches to Mir closed
	2306	Hatches closed (MR)
1997 Oct 3	1728:15	Undocked from SO
	1735s	Pause 27m below Mir
	1740s	Resume flyaway
	1753s	Pause at 90m
	1758s	Resume
	1808s	180m below Mir
	1813s	Reapproach to 75m
	1836s	Stationkeep at 73m
	1930	Begin flyaround, 46min
	1940	Observed Spektr air pulse test
	2003	Second air pulse test
	2016	Sep burn (not in MR)
	2225:27	OMS-6 Sep2 burn 19.6s 10m/s
1997 Oct 4	2032:14	SIMPLEX OMS-7 burn, 10s 2.5m/s
1997 Oct 5	1916	PLBD closed
		Deorbit cancelled
	2343	PLBD opened
1997 Oct 6	1806	PLBD closed	91.90 353 x 381 x 51.7
	2047:45	OMS DO 3:15 104.9m/s	-3 x 381 x 51.7
	2123	EI
	2155:12	Landed at KSC RW15 10d19h20:50
	2155:19	NGTD
	2156:31	WS 10:19:22:12

Soyuz 36

 1980-041A

---

Soyuz-36 (7K-T No. 52) was launched in May 1980 carrying Valeriy Kubasov and Bertalan Farkas. Farkas was a Lt. Col. in the Magyar (Hungarian) Air Force. The ship docked with Salyut-6's rear port; the crew left it there for use by the EO-4 host crew, Leonid Popov and Valeriy Ryumin, who moved it to the front port. Soyuz-36 was then used to return the Soviet-Vietnamese crew to Earth at the end of July.

Soyuz-36
Date	Time	Event	Orbit
1980 May 26	1820:39	Launch by Soyuz-U	KB
	1822	Blok BVGD sep
	1824	Blok A sep
	1829	Blok I MECO
	1830	Blok-I sep	88.99 191 x 264 x 51.60
	2200		90.09 250 x 313 x 51.62
1980 May 27	1620	TCM coelliptic
	1957	Docked Salyut-6 +X
	2006	Hard dock
	2301	Hatch open, crew to Salyut
1980 Jun 4	1445	EO-4 crew to Soyuz
	1608	Undocked +X
	1839	Docked -X
	1920	EO-4 crew to Salyut
1980 Jul 31	0852	EP-4 crew to Soyuz, HC
	1152	Undocked -X
	1425	Deorbit
	1429	DO CO
	1446?	Modules sep
	1451?	Entry
	1515:02	Landed 180 km SE of Dzezkazgan

Apollo 16 (Orion)

  1972-031C

---

Lunar Module 11 `Orion' was the second J-class LM to fly, on the Apollo 16 mission to the Descartes Highlands. Crew of Orion were Capt. John Young, USN and Lt-Col Charles Duke, USAF.

Orion landed at Cayley-Descartes, 8.99S 15.51E.

Duke: `Contact. Stop. PRO. ENGINE ARM. Wow - wild, man! Look at that!' Young: `Pro. Engine Arm. Descent Engine Command Override. Okay, 413'. Duke: `Check the APS'. Young: `Well, we don't have to walk far to pick up rocks, Houston. We're down among them'.

After a sleep period, Young began the mission's first moonwalk. `There you are - mysterious and unknown Descartes Highland Plains. Apollo 16 is going to change your image. I'm sure glad they got ol' Brer Rabbit, here, back in the briar patch where he belongs'.

Orion
Date	Time	Event	Orbit
1972 Apr 16		Launch by Saturn V (SA-511)	KSC LC39A
	2153:15	Extracted from S-4B-511 by CSM 113
1972 Apr 18	0300	Checkout
	0500	Power down
1972 Apr 18	2324	Checkout
1972 Apr 19	0100?	Power down
1972 Apr 20	1501	Crew entry, power up
	1808	Undocked from CSM 113	19 x 110
		RCS burn
1972 Apr 21	0211:25	DPS burn, PDI 2.04km/s
	0223:35	Landed at Descartes Base
1972 Apr 21	1647:33	LEVA-1 begin depress
	1648:02	At 1psi
	1648:36	At 0.5 psi
	1649:34	HO
	1654:45	CDR egress
	1655?	Jettison bag
	1658:05	CDR on surface
	1659	LMP egress
	1700	LMP on surface
	1716	LRV-2 deployed
	1815	ALSEP packages removed from LM
	1827	LMP carrying ALSEP
	1845?	ALSEP deploy
	2001	Geophone charge fired
	2002:38	Geophone
	2003:19	Geophone
	2003:53	Geophone
	2004:49	Geophone 5
	2005:28	Geophone 6
	2006:15	Geophone 7
	2006:50	Geophone 8
	2008+	Geophone 9-18
	2015	Geophone 19
		Traverses
	2334	LMP ingress
	2355	CDR ingress
	2356:52	HC
	2357:50	Begin repress
	2358	(CDR 07:00, LMP 06:43)
	2358:18	2 psi
	2358:40	3.5psi?
1972 Apr 22	0000	Hatch locked (was closed at 2356)
	1633:25	Depress 3.5psi for LEVA-2
1972 Apr 22	1633	LEVA-2
	1634:41	Depress at 0.3psi
	1635	HO
	1639	CDR egress
	1640	Jett bag
	1641	CDR on surface
	1642	LMP egress
	1643	LMP on surface
		LRV to Stone Mountain
	2344	LMP ingress
	2347	Unid object jettisoned
	2353	CDR ingress
	2355:27	HC and locked
	2355:55	Begin repress
	2356:06	Pressure at 1psi
	2356	At 3.5psi, 7:23:26
1972 Apr 23	1525:20	LEVA-3 at 3.5psi
	1526	At 0.7psi?
	1527:25?	HO
	1531	CDR egress
	1532:05?	Jett bag
		(CWGs, LCGs, sleep restraints)
	1532	CDR on surface
	1533	LMP on porch
	1534	LMP on surface
		Traverse to North Ray Crater
	2054	LMP ingress
	2102	CDR ingress
	2103:47	HC and locked
	2105	Repress (depress/3.5psi 05:40)
		Cdr 05:30, LMP 05:19
	2213:09	Begin ED depress
	2213:42	At 1 psi
	2213:59	At 0.5psi
	2215:08	HO
	2215	PLSS ejected
	2216	PLSS and ISS jett bag ejected
	2216:53	HC and locked
	2217	Repress
		Hatch closed, repress (00:05?)

Orion
Date	Time	Event	Orbit
1972 Apr 24	0125:48	Launch from LM11 DS, Descartes
		LM mass 4965 kg
	0132:56	DPS shutdown,LOI	15 x 74
			16 x 78 (PAO)
	0136:18	RCS tweak 3m/s
	0220:05	TPI 23m/s	74 x 119
	0302:42	TPF 9m/s, Rendezvous CSM 113 at 0.5km
	0310	Stationkeeping with CSM
	0334	Soft dock
	0335:18	Docked with CSM 113
	0410?	HO
		Crew transfer to CSM
	2030?	HC
	2054:12	Undocked, tumbling	100 x 126
		Mass 2392 kg
1972 Apr 25	1200?	End of transmissions

STS-90 (Columbia)

 1998-022A

---

STS-90 carried Neurolab, the final Spacelab mission. The first attempt to launch was scrubbed prior to tanking on Apr 16 when a network signal processor, used to relay data to TDRS or MILA, failed in tests. Launch the following day went without a hitch. STS-90 was the first test of the OMS Assist Maneuver, in which the OMS engines are fired shortly after SRB separation to provide extra payload capacity to orbit.

The Spacelab payload carried a variety of life sciences experiments. The BDS carried human renal cells and leukemia cells for study. On Apr 25 the CO2 system (RCDRS, Regenerative Carbon Dioxide Removal System) failed, threatening an early return. However, the system was soon fixed and the mission continued. An unexpectedly large number of the baby rats died during the mission, but otherwise the flight was completed smoothly.

STS-90
Date	Time	Event	Orbit
1998 Mar 16	1550	Roll to VAB
1998 Mar 23	1230	Roll to LC39B
1998 Apr 16	1215	Scrub with computer failure
1998 Apr 17	1819:00	Launch by Shuttle from LC39B
	1821:01	SRB sep
	1821:15	OMS assist burn, 1:42
	1822:58	OMS cutoff
	1827:28	MECO	78 x 280 x 39.0
			76 x 273 x 39.0 (STS-MR)
	1827:48	ET sep
	1900:27	OMS-2 1:50 52.1m/s
	1902:18	OMS-2 CO	257 x 286 x 39.0
	1956	PLBD open
1998 Apr 21			89.90 256 x 282 x 39.0
1998 Apr 22	2014:00	RCS orbit adjust 1 15s 1m/s	89.86 253 x 282 x 39.0
1998 Apr 25	0345	CO2 scrub system failed
1998 Apr 26		System repaired
1998 Apr 27	1828:59	RCS orb adj 2 7s 0.5m/s	89.80 249 x 278 x 39.0
1998 May 3	1235	PLBD closed	89.72 247 x 274 x 39.0
	1510:10	OMS DO 2:19 64.9m/s
	1512:30	OMS DO CO	87.53 31 x 272 x 39.0
	1537:14	Entry interface
	1608:59	MGTD KSC RW33, 15:21:49:59
	1609:13	NGTD
	1609:58	Wheels stop
	2230	Tow to OPF/3

Globalstar 25

 1999-031A

---

The third Globalstar Delta flight carried M052, M049, M025 and M047. Spacecraft mass was 448 kg each, dispenser mass was 269 kg for a total cargo of 2061 kg.

Globalstar
Date	Time	Event	Orbit
1999 Jun 10	1348:43	Launch by Delta 7420-10	CC LC17B
		T+1:03 SRM 1-4 out
		T+1:07 SRM 1-4 sep
		T+4:24 MECO
		T+4:37 SES
		T+4:47 Fairing sep
	1400:01	T+11:18 SECO-1	185 x 1361 x 51.9
	1450:35	T+1:01:52 SES-2
	1451:01	T+1:02:18 SECO-2	1367 x 1367 x 52.0
	1457:53	T+1:09:10 U1/U2 deploy
	1502:03	T+1:13:20 L1/L2 deploy
	1503	T+1:15 Stage 2 ullage
	1537:03	T+1:48:20 SES-3 evasive
		T+1:48:25 SECO-3	1010 x 1373 x 51.3
	1544:33	T+1:55:50 SES-4 depletion
		T+1:55:56 SECO-4	810 x 1370 x 51.5
1999 Jun 12			113.16 1362 x 1380 x 52.0
1999 Jun 16		Orbit raise
1999 Jun 19			114.06 1411 x 1413 x 52.0

Gorizont 29

 1993-072A

---

Gorizont No. 41 (the 30th to reach orbit) was launched by NPO PM for the Rimsat consortium based in Fort Wayne, Indiana. It was also known as Rimsat-1.

Philippine Agila Satellite Inc (PASI) of Manila leased Gorizont No. 41 in Jan 1997 and moved it to 161 E in Mar 1997. It was then renamed PASI 1 or PASI/Agila 1.

In late 1998 it was again sold to Lockheed Martin Intersputnik and moved to 130E as satellite LMI AP-1.

Gorizont 41
Date	Time	Event	Orbit
1993 Nov 18	1354:59	Launch by Proton-K	KB
	1404	Stage 3 sep	191 x 192 x 51.7
	1512?	DM2 burn 1	315 x 35052 x 57.3
	2028?	DM2 burn 2
	2032?	Blok-DM2 No. 85L sep
1993 Nov 18			1399.59 35038 x 35099 x 1.5 GEO 87.9E+9.4E
1993 Nov 28		mv in	1436.04 35758 x 35812 x 1.5 GEO 130.1E
1994 Jan 1			1435.97 35768 x 35800 x 1.4 GEO 129.8E
1994 Oct 11			1436.05 35782 x 35788 x 0.8 GEO 130.3E
1995 Oct 29			1436.05 35780 x 35791 x 0.2 GEO 130.3E
1997 Jan		Lease by PASI as PASI 1
1997 Feb 1		mv out	1435.93 35776 x 35789 x 1.0 GEO 129.9E
1997 Mar 8		mv in	GEO 161E
1997 Mar 14			1436.12 35783 x 35790 x 1.1 GEO 160.9E
1997 Nov 18			1436.06 35768 x 35803 x 1.6 GEO 160.6E
1998 Oct 25			1436.13 35771 x 35803 x 2.3 GEO 160.6E
1998 Nov 20		mv out	1438.35 35710 x 35850 x 2.3 GEO 158.6E+0.5W
1998 Nov		Lease to LMI as AP-1
1999 Jan 14		mv in	GEO 129.50E
1999 Feb 23			1436.09 35759 x 35813 x 2.5 GEO 130.4E
1999 Oct 17			1436.19 35780 x 35796 x 3.0 GEO 130.1E