The Dictionary of Global Culture : What Every American Needs to Know as We Enter the Next Century--From Diderot to Bo Diddley

 https://welib.org/md5/71172eb4a01ee4a39a94417fd855b677

SMS 1

  1974-033A

---

Synchronous Meteorological Satellite 1 was launched at 0931 on 1974 May 17 by Delta 2914 from Cape Canaveral. The Thor first stage shut down prematurely at 0935 after a LOX tank pressure loss; the Delta burned from 0935 to 0940 and reached a 155 x 213 km x 28 deg parking orbit with insufficent propellant to make its second 8s burn. After a 14 minute coast, the Star 37E third stage ignited at 0954. After it separated at 0956, SMS 1 was in a 182 x 33250 km x 24 deg transfer orbit, significantly lower in apogee than planned. The solid SVM-5 apogee motor fired at 0700 on May 19, and was followed by 9 daily thruster burns to raise the altitude. Finally on Jun 4 SMS 1 was near geostationary at 86 deg W. After a brief checkout it was stationed at 45W for GATE (the GARP Atlantic Tropical Experiment). SMS 1 was turned over to NOAA for operational use on 1974 Dec 10 despite problems with the S-band transmitter. By 1975 Oct it had been moved back to 75 W, which was to become the operational GOES East position. In early 1976 it was moved to 105W as a standby satellite, after being replaced by GOES 1. On 1979 Jan 26 it arrived at the GOES E position to replace GOES 2 in the First GARP Global Experiment (FGGE), but after SMS 1 had S-band transmitter problems in April GOES 2 took over again and SMS 1 moved to the side. SMS 1 spent 1980 at 131W backing up the GOES W position. On 1981 Jan 29 the orbit was raised by 500 km and SMS 1 was decommissioned a few days later.

SMS 1
Date	Time	Event	Orbit
1974 May 17	0931:00	Launch by Delta 2914
		T+0:59 SRM 7-9 on
		SRM 1-6 sep
		SRM 7-9 sep
	0934:48	T+3:48 MECO
	0935	Thor sep
	0935:01	T+4:01 Delta SES-1 burn 5:13
	0940:14	Delta SECO-1	155 x 213 x 28
	0952?	SES-2 burn
	0954?	Stage 2 sep
	0954:15	T+23:15 Star 37E burn 44s?
	0955:59?	Star 37E burnout
	0957:14?	Star 37E sep	182 x 33250 x 24.52
1974 May 19	0700	SVM-5 fired 40s; GEO 56 deg/d
1974 May 19?		SVM-5 ejected	30823 x 32860 x 2?
1974 May 20		Raise orbit OTM-1
1974 May 21		Raise orbit OTM-2
1974 May 22		Raise orbit OTM-3
1974 May 23		Raise orbit OTM-4
1974 May 24		Raise orbit OTM-5
1974 May 24?		Cooler cover eject
1974 May 24		First test images
1974 May 25		Raise orbit OTM-6
1974 May 26	2130	First operational image
1974 May 26		Raise orbit OTM-7
1974 May 27		Raise orbit OTM-8
1974 May 28		Raise orbit OTM-9
1974 Jun 4		On station	GEO 60W dr
1974 Jun		Checkout
1974 Jun			45W
1974 Dec 10		To NOAA
1975 Oct		GOES E	75W
1976 Jan		Move to standby, replaced by GOES 1	GEO 105W
1977 Jan 26			1436.08 35705 x 35876 x 2.3 GEO 104.4W
1978 Feb 11			1436.11 35782 x 35791 x 3.0 GEO 106.1W
1978 Jul 24			1436.09 35761 x 35811 x 3.3 GEO 105.3W
1978 Aug 7		Mv out	1433.55 35710 x 35763 x 3.3
1978 Aug 24			1436.02 35761 x 35808 x 3.4 GEO 90.1W
1978 Dec 7			1436.32 35773 x 35808 x 3.6 GEO 91.4W
1979 Jan 11			1431.66 35689 x 35710 x 3.6 GEO 81.8W+1.1E/d
1979 Jan 26		GOES E, replacing GOES 2
1979 Feb 8			1436.17 35720 x 35855 x 3.7 GEO 74.5W
1979 Apr		Replaced by GOES 2
1979 Apr 25		mv out	1434.05 35734 x 35759 x 3.8 GEO 74.8W+0.5W
1979 May 7		mv in	1436.02 35766 x 35803 x 3.8 GEO 69.9W
1979 Sep 29			1436.20 35729 x 35847 x 4.1 GEO 68.1W
1979 Nov 3			1436.17 35721 x 35854 x 4.2 GEO 70.2W
1979 Nov 5			1438.15 35802 x 35850 x 4.2 GEO 86.0W+0.5W
1980 Mar 2			1437.15 35787 x 35827 x 4.5 GEO 126.8W+0.3W
1980 May 7			1436.36 35783 x 35800 x 4.6 GEO 132.6W+0.07W
1980 May		GOES W backup
1981 Jan 29	0600		1436.00 35777 x 35792 x 5.2 GEO 130.8W
1981 Jan 29		Orbit raise
1981 Feb 3		End of ops
1981 Mar 17			1435.76 35766 x 35793 x 5.3 GEO 128.1W
1984 Sep 25			1460.24 36199 x 36316 x 8.1 GEO 171.5E+6.0W
1990 Jan 4			1460.23 36206 x 36308 x 12.7
1995 Dec 24			1460.27 36187 x 36328 x 16.5
1998 Aug 4			1460.23 36181 x 36333 x 17.2

Payload:

• VISSR Visible/InfraRed Spin Scan Radiometer, with 0.55-0.75,10.5-12.6 mu bands.

• DCS Data Collection System

• SEM Space Environment Monitor, containing

  • EPM Energetic Particle Monitor

  • SXM Solar X-ray monitor

Aviation Week: August 6,2001

 https://welib.org/md5/3bf3ff7daab2bf285579e54aba9020fe

Town and Country: June 2001

 https://welib.org/md5/cc22ee081b49185caeab78eb0049196d

Jumpseat 5

 1978-021A

---

SDS 3
Date	Time	Event	Orbit
1978 Feb 25	0500?	Launch by Titan 34B Agena D	V SLC4W
	0502?	Stage 2 burn
	0505?	Stage 2 MECO
	0506?	Agena MES-1
	0510?	Agena MECO-1	180? x 500? x 63
	0536?	Agena MES-2
	0538?	Agena MECO-2
	0540?	Agena sep	702.8 311 x 39377 x 63.2 (UN)

Orbital Debris: A Chronology

 https://ntrs.nasa.gov/api/citations/19990041784/downloads/19990041784.pdf

Kosmos 489

  1972-035A

---

Kosmos-489 was the last of the Tsiklon satellites to be launched to a 74 degree orbit.

Kosmos-489
Date	Time	Event	Orbit
1972 May 6	1124:51	Launch by 11K65M	PL
	1130	Stage 2 burn
	1137?	Stage 2 coast
	1227?	Stage 2 burn 2
	1228?	Stage 2 sep
	2130		104.82 969 x 1002 x 74.02

Navstar 35

 1993-054A

---

Navstar SVN 35 was launched on 1993 Aug 30. It was placed in plane B-4 with identification PRN 05. It was the first launch to carry a laser retroreflector.

Navstar 35
Date	Time	Event	Orbit
1993 Aug 30	1238:00	Launch by Delta 7925	CC LC17
		T+0:56 SRM 1-3,7-9 out
		T+1:01 SRM 4-6 on
		T+1:02 SRM 1-3 sep
		T+1:03 SRM 7-9 sep
		T+1:57 SRM 4-6 off
		T+2:02 SRM 4-6 sep
		T+4:25 MECO
		T+4:31 VECO
		T+4:33 Stage 1 sep
	1242	Stage 2 TIG (T+4:38)
	1242	Fairing sep (T+4:50)
	1248?	T+10? Delta SECO-1	185 x 185 x 34.0
	1258?	T+20? Delta SES-2
	1258?	T+20? Delta SECO-2	185 x 721
	1259?	Delta sep from GPS/PAM-D
	1300?	T+22? TES
	1302?	T+24? TECO
	1303?	T+25? PAM-D sep	194 x 20317 x 34.8
	1343?	SES-3 depletion	451 x 721 x 22.0
1993 Sep 2	0337?	Star 37XFP burn	713.73 19914 x 20240 x 55.0
1993 Sep 28		In service
1997 Feb 1		Operating at slot B-4

ARGOS

 1999-008A

---

[P91-11999-08A

The P91-1 ARGOS satellite was launched in 1999 Feb by Delta from Vandenberg. Orbit will be 900 x 900 km x 98.7 deg. ARGOS (Advanced Research and Global Observation Satellite) is built by Boeing (fka Rockwell) Seal Beach, for the USAF. The largest experiment is the ESEX arcjet thruster, with a power of 30 kW. It will be used for system tests but will not alter the spacecraft's orbit. Mass is 2490 kg. The USA experiment, using SPTN-1 proportional counters, will carry out very long (1 month) exposures on bright X-ray sources for time variability studies.

Argos is managed by the Tri-Service Spacecraft Div., STP, Kirtland AFB.

A first launch try on Jan 28 failed when a vernier engine did not ignite.

ARGOS
Date	Time	Event	Orbit
1999 Jan 28	1044:44	Launch abort T-2s	V SLC2
1999 Feb 23	1029:55	Launch by Delta 7920-10
		T+1:04 SRM1-6 burnout
		T+1:05 SRM7-9 burn
		T+1:26 SRM1-3 sep
		T+1:29 SRM4-6 sep 28 km	-6340 x 32 ?
		T+1:30 dogleg
		T+2:09 SRM7-9 burnout
		T+2:11 SRM7-9 sep 55 km	-6200 x 75 ?
		T+4:23 MECO
		T+4:31 Stage 1 sep
		T+4:37 SES-1 129 km	-4140 x 170 ?
		T+4:42 Fairing sep 132 km	-4120 x 170 ?
	1040:53	T+10:58 SECO-1	178 x 852 x 98.84
	1121:17	T+51:22 SES-2
	1121:37	T+51:42 SECO-2
	1128:15	T+58:20 Stage 2 sep from ARGOS	843 x 843 x 98.7
		T+58:20 Stage 2 retro
	1145:55	T+1:16:00 SES-3 evasive
		T+1:16:06 SECO-3 evasive	620 x 850 x 98.20
	1201:39	T+1:31:44 SES-4 depletion
	1202:05	T+1:32:10 SECO-4	620 x 850 x 96.7
	1209:55	T+1:40:00 Orsted and SUNSAT sep	649 x 863 x 96.5

Payload:

• CERTO Coherent Radio Topography Experiment Payload, NRL

• CIV Critical Ionization Vel experiment, Phillips Lab

• ESEX Electric Propulsion for Space Test TRW/Philips arcjet thruster

• ESEX NaS batteries (3)

• SUPER Survivable Power Subsystem Demonstrator Solar Power module

• EUVIP EUV Imaging Photometer, UCB for plasmasphere background.

• GIMI Global Imaging Monitor of the Ionosphere, NRL UV imager radiometer for daily O+ and e- density, 750-2000A. high time resolution studies 1-15 keV)

• HIRAAS High Res Airglow/Aurora Spectroscopy, NRL, with UV spectrographs. (Rocket experiment reflight)

• LORAAS Low Res Airglow and Auroral Spectrograph, NRL (SSULI prototype)

• HTSSE II High Temp Superconducting Expt., NRL

High school 411

 https://welib.org/md5/815d101f96b0b2d9279b26a8e1f554d7

Kosmos 866

 1976-110A

---

Kosmos-866
Date	Time	Event	Orbit
1976 Nov 11	1045	Launch by Soyuz-U	Baikonur
	1049	Blok-I burn
	1053	Blok-I sep
1976 Nov 11			89.15 178 x 286 x 65.0
1976 Nov 12			89.11 176 x 285 x 65.0
1976 Nov 14			89.43 176 x 315 x 65.0
1976 Nov 18			89.33 174 x 308 x 65.0
1976 Nov 20			88.46 171 x 224 x 65.0
1976 Nov 22			88.38 170 x 218 x 65.0
1976 Nov 23
	0739?	Deorbit
	0749?	PO sep
	0753?	Entry
	0809?	Landed

Us Weekly: June 4,2001

 https://welib.org/md5/df980633994f002919c4eee6b3788dca

Soyuz TM-17 (Sirius)

 1993-043A

---

7K-STM 11F732 No. 66 (Soyuz TM-17) was launched in Jul 1993 to ferry a crew to the Mir station.

Soyuz TM-17, Flight 1
Date	Time	Event	Orbit
1993 Jul 1	1432:58	Launch by Soyuz-U2	KB
	1434:50	Blok BVGD sep
	1437:42	Blok A sep
	1441:43	Blok I sep	201 x 242 x 51.6
	1812:53	TCM-1 14s
	1905:40	TCM-2 21s	219 x 372 x 51.6
1993 Jul 2			219 x 372 x 51.6 (TASS)
	1519	TCM-3 18s	227 x 371 x 51.6
1993 Jul 3	1356:19	TCM-4 57s
	1441:50	TCM-5 56s
	1540	Range 400m, 1.8 m/s
	1548	Range 180m to Mir
	1624:03	Docked with Mir -X
	1745	Hatch opened

Soyuz TM-17, Flight 2
Date	Time	Event	Orbit
1994 Jan 14	0154	Hatch closed
	0437:11	Undocked Mir -X
	0441	Range 30 m
	0443	Mir close up camera survey
	0447	Minor collision with Mir
	0450?	Sep from Mir
	0723:46	Deorbit burn, 406 km alt.
	0751:52	BO, PAO sep
	0756	Entry interface, 7.6 km/s
	0818:20	Landed

Kosmos 345

  1970-039A

---

Zenit-4 No. 82 was launched on 1970 May 20. It flew an 8 day mission at 51.8 deg from Baikonur.

Kosmos-345
Date	Time	Event	Orbit
1970 May 20	0920:01	Launch by 11A57	KB
	0924	Blok I burn
	0929	Blok-I sep
	1803		89.16 193 x 271 x 51.8
1970 May 21	1152		89.13 192 x 270 x 51.8
1970 May 26	1159		88.95 187 x 257 x 51.8
1970 May 28	0832?	Retrofire
	0852?	Landed after 7.98d

Encyclopedia of the Scientific Revolution: From Copernicus to Newton

 https://welib.org/md5/2aacfdaffe51e2106d477ed2e1382f4e

Kosmos 296

  1969-075A

---

Zenit-4 No. 68 flew a 65.0 degree Baikonur mission in Aug-Sep 1969.

Kosmos-296
Date	Time	Event	Orbit
1969 Aug 29	0905:00	Launch by 11A57	KB
	0909	Blok-I burn
	0914	Blok-I sep
	1026		89.59 201 x 306 x 65.0
1969 Aug 31	0500		89.59 207 x 302 x 64.95
1969 Sep 4	0815		89.50 205 x 294 x 65.0
1969 Sep 5	0657?	Blok-I reentered
1969 Sep 6	0625?	Retrofire
	0648?	Landed after 7.90d

Spaceflight: June 2001

 https://welib.org/md5/11758038ca4b2a74e494c3e57d06e8fa

Lunar Prospector

 1998-001A

---

Lunar Prospector was selected in Mar 1995 as part of the Discovery program. It will be built and operated by Lockheed Missiles and Space Co/Sunnyvale; NASA oversight of the project is managed by NASA-Ames which also controls the probe.

The spacecraft is a spin stabilized solar-panel-covered cylinder 1.4m dia, 1.22m high surrounding a triangular inner structure based on the Iridium satellite, and has a hydrazine propulsion system with six Olin MR-106E 22N thrusters with total mission impulse of at least 239 kNs. Three booms unfold to carry the experiments, a magnetometer boom 3.8m long and two instrument booms 2.5m long. Mass is 158 kg dry, 296 kg fuelled. The spacecraft carried a special Celestis capsule with some of the ashes of lunar scientist Gene Shoemaker, who died in a car accident the previous year.

Launch was Jan 1998 by LMA Athena-2 with a Model 92 fairing (92 inch diameter) from Cape Canaveral's Florida Spaceport Authority LC46. It will be inserted in a 100 x 100 km, 118 min lunar polar orbit. The Athena-2 has two Castor 120 stages, an Orbus 21D Equipment Section Boost Motor, and an Orbit Adjust Module.

As well as the LP payload, Athena-2 carries a TLI stage. The TLI stage is built around a Thiokol Star 37FM (TE-M-783-7) solid motor and a Thiokol graphite interstage adapter. The TLI Stage is 0.17m long and 0.21m in diameter with a fueled mass of 1227 kg and an empty mass of 212 kg. (The Star 37FM has thrust 45.8 kN, impulse 2894 kNs and burn time 63s, with diameter 0.94m and length 1.68m). The TLI stage also has spinup motors which fire prior to LP separation to spin-stabilize the LP.

Launch mass of S/C + TLI stage is 1523 kg.

The neutron spectrometer will help in the search for hydrogen and water ice; the alpha particle spectrometer will detect outgassing events. 

In 1998 preliminary evidence was reported for substantial amounts of ice at the lunar poles.

End of mission in 1999 will have impact at 42E 87.7S.

According to Alan Binder's book on LP the TLI stage reentered over the Indian Ocean 'several days after launch'. First perigee may have been around 2030 UTC Jan 15.

LP
Date	Time	Event	Orbit
1998 Jan 7	0228:44	Launch by LMLV-2	SPFL LC46
		T+01:29 Stage 1 (Castor 120) sep, 18 km
		T+01:29 Stage 2 burn
		T+03:00 Stage 2 (Castor 120) sep, 95 km
		T+03:52 Fairing sep, 132 km
		T+03:57 Stage 3 (Orbus 21D) burn, 134 km
	0235:15	T+06:31 Stage 3 sep, 156 km
	0235:15	T+06:31 OAM burn 418s
	0242:13	T+13:29 OAM cutoff, injection 156 km
		Parking orbit	153 x 202 x 29.2
		OAM orient for TLI
	0323:57	T+55:13, U+0:00 OAM sep	141 x 198 x 29.3
	0323:58	U+0:01 TLI stage spinup
	0324:17	U+0:20 TLI burn
	0325:20	U+1:23 TLI burnout - MET 0
	0325:26	U+1:29 TLI stage sep
	0524	TLI sep confirmed
			197 x 352645 x 29.20
1998 Jan 7	0630	Mag boom deploy
	0709	Booms deploy
	0730	Booms extended
	0920?	OAM reentered?
			76 x 381571 x 29.3
	1155	MCM-1 burn 13.0m/s axial, 49m/s tgtl.
	1840	Pass EL1:4
	1851	TLI stage pass EL1:4?
1998 Jan 8	0825	MCC-2, 8.4m/s
			-267 x 379973 x 29.3
1998 Jan 10	1812	Enter L sphere	73 x -17841 x 89.7
1998 Jan 11	0156	Equigravisphere
1998 Jan 11	1145	LOI burn, 32 min
1998 Jan 11	1217	LOI, 12 hr orbit	84 x 8470 x 89.72
	1740	Capture correction
1998 Jan 12	1058	LOI-2, 27 min to 3.5 hr period	87 x 1861 x 89.9
	1125	End of burn
1998 Jan 13	1206	LOI-3, 118 min op orbit	120.01 92 x 153 x 90.0
1998 Jan 15	2144	76s trim	92 x 100 x 90.1
	2206	16s trim	99 x 100 x 90.1
	2357	Move to mapping attitude
1998 Jan 16			117.88 99 x 101 x 90.6
1998 Jan 22	0000		118.0 80 x 120 x 90.1
1998 Jan 24	0000		118.0 90 x 110 x 90.1
1998 Jan 27	0000		118.0 88 x 112 x 90.1
1998 Jan 30	0000		118.0 86 x 114 x 90.1
1998 Feb 2	1800		118.0 96 x 104 x 90.1
1998 Feb 10	0000		118.0 92 x 109 x 90.1
1998 Feb 19	0000		118.0 85 x 115 x 90.3
1998 Mar 6	0000		118.0 82 x 117 x 90.0
1998 Mar 8	0349	OTM-1a periselene raise
1998 Mar 8	0453	OTM-1b aposelene lower
1998 Mar 12	0000		118.0 94 x 106 x 90.7
1998 Mar 19	0000		118.0 84 x 115 x 90.4
1998 Apr 2	0000		118.0 93 x 105 x 90.2
1998 Apr 16	0000		118.0 87 x 110 x 90.0
1998 Apr 23	0000		118.0 82 x 118 x 90?
1998 May 1			118.0 85 x 114 x 90?
1998 May 1	1550	Circ burn 38s	118.0 112 x 114 x 90
1998 May 1	1654	Circ burn, exchange peri 37s	88 x 112 x 90
1998 May 5	0000		118.0 88 x 112 x 90.9
1998 May 15	0000		118.0 86 x 114 x 90?
1998 Jun 25			83 x 118 x 90
1998 Jun 25	2142	MOC periapsis raise	109 x 118 x 90
	2246	MOC apo lower	90 x 109 x 90
1998 Jun 26	0000		118.0 90 x 110 x 89.8
1998 Jul 10	0000		118.0 90.2 x 108.6 x 89.9
1998 Nov 13	1800		118.0 93 x 106 x 90.0
1998 Dec 4	1800		118.0 91 x 109 x 90
1998 Dec 19	1740		77 x 122 x 90
1998 Dec 19	1811	Lower orbit, 47s	50 x 77 x 90
1998 Dec 19	1911	Lower orbit, 150s	112.0 25 x 55 x 90
1998 Dec 30	0000		112.0 29 x 52 x 90
1999 Jan 8	0000		112.0 31 x 49 x 90
1999 Jan 15	1800		112.0 30 x 50 x 90
1999 Jan 29	0655	40s burn	43 x 63 x 90
	0743	71s burn	15 x 45 x 90
	2359		17 x 43 x 90
1999 Feb 3	0000		111.0 21 x 39 x 90
1999 Feb 11	0000		111.0 26 x 33 x 90
1999 Feb 19	0000		111.0 20 x 40 x 90
1999 Feb 25			16 x 40 x 90
1999 Feb 25	1116	Orbit raise	40 x 44 x 90
	1155	Orbit lower	15 x 44 x 90
1999 Mar 5	0000		111.0 27 x 32 x 90
1999 Mar 12	0000		111.0 23 x 36 x 90
1999 Mar 19	0000		111.0 15 x 45 x 90
1999 Mar 25	1730	Orbit burn EMOC-3 43s
	1810	Orbit burn EMOC-3 47s	111.0 15 x 45 x 90
1999 Apr 2	0000		111.0 27 x 32 x 90
1999 Apr 9	0000		111.0 22 x 37 x 90
1999 Apr 16	0000		111.0 12 x 47 x 90
1999 Apr 20	0132	Orbit burn EMOC-4 45s, 7m/s
	0214	Orbit burn EMOC-4 45s, 7m/s
1999 Apr 23	0000		111.0 21 x 38 x 90
1999 Apr 30	0000		111.0 23 x 36 x 90
1999 May 5	1735	Orbit burn EMOC-5 25s, 4m/s
	1833	Orbit burn EMOC-5 26s, 4m/s
1999 May 7	0000		111.0 21 x 38 x 90
1999 May 14?	0000		111.0 19 x 41 x 90
1999 May 21	0000		111.0 17 x 43 x 90
1999 May 28	0000		111.0 17 x 42 x 90
1999 Jun 1	2340	Orbit burn EMOC-6 45s 7m.s
1999 Jun 2	0051	Orbit burn EMOC-6 45s 7m/s
1999 Jun 4	0000		111.0 17 x 42 x 90
1999 Jun 11	0000		111.0 17 x 42 x 90
1999 Jun 18	0000		111.0 14 x 46 x 90
1999 Jun 25	0000	111.0 18 x 42 x 90
1999 Jun 29	1511	Orbit burn EMOC-7 47s 7m/s
1999 Jun 29	1622	Orbit burn EMOC-7 46s 7m/s
1999 Jul 1	0000	111.0 17 x 42 x 90
1999 Jul 9	0000	111.0 18 x 42 x 90
1999 Jul 16	0000	111.0 19 x 41 x 90.0
1999 Jul 23	0000	111.0 20 x 39 x 90.0
1999 Jul 26	1401	Orbit burn 9s, 1.4m/s
1999 Jul 28		Lunar eclipse	111.0 11 x 49 x 90.0
1999 Jul 30	0815	Apogee raise 40m/s, 256s
	2200		120.0 17 x 234 x 90.0
1999 Jul 31	0900	LOS, to farside
1999 Jul 31	0915:55	Lower periapsis negative, -44m/s, 4:36	-163 x 234 x 90
1999 Jul 31	0952:00	Impact in Mawson 87.7S 42.1E
		1.7 km/s at 6 deg, mass 158 kg

Payload:

• Neutron spectrometer (on mast) (LANL)

• Gamma ray spectrometer (LANL)

• Alpha particle spectrometer (on mast ) (LANL/LM)

• Magnetometer and electron spectrometer (MAG/ER) (UCB)

Riding To Win

 https://welib.org/md5/b699f44110f75b8546e108411b30c295

Kosmos 880

  1976-120A

---

This was the I-2M satellite that served as a target for Kosmos-886.

Kosmos-880
Date	Time	Event	Orbit
1976 Dec 9	2000	Launch by 11K65M	PL
	2008?	Stage 2 MECO-1
	2033?	Stage 2 MECO-2, sep
1976 Dec 9			96.4 560x617x65.9