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Table of Artificial Satellites Launched in 1979

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Table of Artificial Satellites Launched in 1979 This electronic version (PDF) was scanned by the International Telecommunication Union (ITU) Library & Archives Service from an original paper document in the ITU Library & Archives collections. La présente version électronique (PDF) a été numérisée par le Service de la bibliothèque et des archives de l'Union internationale des télécommunications (UIT) à partir d'un document papier original des collections de ce service. Esta versión electrónica (PDF) ha sido escaneada por el Servicio de Biblioteca y Archivos de la Unión Internacional de Telecomunicaciones (UIT) a partir de un documento impreso original de las colecciones del Servicio de Biblioteca y Archivos de la UIT. (ITU) ﻟﻼﺗﺼﺎﻻﺕ ﺍﻟﺪﻭﻟﻲ ﺍﻻﺗﺤﺎﺩ ﻓﻲ ﻭﺍﻟﻤﺤﻔﻮﻇﺎﺕ ﺍﻟﻤﻜﺘﺒﺔ ﻗﺴﻢ ﺃﺟﺮﺍﻩ ﺍﻟﻀﻮﺋﻲ ﺑﺎﻟﻤﺴﺢ ﺗﺼﻮﻳﺮ ﻧﺘﺎﺝ (PDF) ﺍﻹﻟﻜﺘﺮﻭﻧﻴﺔ ﺍﻟﻨﺴﺨﺔ ﻫﺬﻩ .ﻭﺍﻟﻤﺤﻔﻮﻇﺎﺕ ﺍﻟﻤﻜﺘﺒﺔ ﻗﺴﻢ ﻓﻲ ﺍﻟﻤﺘﻮﻓﺮﺓ ﺍﻟﻮﺛﺎﺋﻖ ﺿﻤﻦ ﺃﺻﻠﻴﺔ ﻭﺭﻗﻴﺔ ﻭﺛﻴﻘﺔ ﻣﻦ ﻧﻘﻼ ً◌ 此电子版（PDF版本）由国际电信联盟（ITU）图书馆和档案室利用存于该处的纸质文件扫描提供。 Настоящий электронный вариант (PDF) был подготовлен в библиотечно-архивной службе Международного союза электросвязи путем сканирования исходного документа в бумажной форме из библиотечно-архивной службы МСЭ. © International Telecommunication Union TELECOMMUNICATION JOURNAL - VOL. 47 - IV/1980 C0SM0S-1101 1979 42B MOLNYA-3 (11) 1979 4 A COSMOS-1102 1979 43 A MOLNYA-3 (12) 1979 48 A A COSMOS-1103 1979 45A D COSMOS-1104 1979 46 A ARIANE-6 1979 104A C0SM0S-1105 1979 52A DMSP-4 1979 50A N ARIEL-6 1979 47A COSMOS-1106 1979 54A DSCS-II 13 1979 98A AYAME 1979 9 A COSMOS-1107 1979 55A DSCS-II 14 1979 98B NOAA-6 1979 57A COSMOS-11 08 1979 56A D C0SM0S-1109 1979 58A F D COSM0S-1110 1979 60 A L. D COSMOS-1111 19 79 61A r BHASKARA 1979 51A COSMOS-1112 1979 63A EKRAN-3 1979 15A BIOSPUTNIK-7 1979 83A PROGRESS-5 1979 22A COSMOS-1113 1979 64A EKRAN-4 1979 87A PROGRESS-6 1979 39A COSMOS-1114 1979 65 A PROGRESS-7 1979 59A COSMOS-1115 1979 66A C COSMOS-1116 1979 67 A rF CORSA-B 1979 14A COSMOS-1117 1979 68A n COSMOS-1118 1979 69A K COSMOS-1070 1979 1 A FLT SATCQM-2 1979 38 A C0SM0S-1071 1979 2 A COSMOS-1119 1979 71 A RADUGA-4 1979 35A COSMOS—1072 1979 3A COSMOS-1120 1979 73A RCA-SATCOM-3 1979 101A COSM0S-1073 1979 6A COSMOS-1121 1979 74A COSMOS-1074 1979 8A COSMOS-1122 1979 75 A G COSMOS-1075 1979 10A COSMOS-1123 1979 76A G0RIZ0NT-2 1979 62A c COSM0S-1076 1979 11A COSMOS-1124 1979 77A GORIZONT-3 1979 105 A v C0SM0S-1077 1979 12A COSMOS-1125 1979 78A SAGE 1979 13A COSMOS-1126 1979 79A COSMOS-1078 1979 16A 1979 7A COSMOS-1127 1979 80 A SCATHA COSMOS-1079 19 79 19A 1979 51A COSMOS-1128 1979 81A H SEO COSMOS-IO8O 1979 23A SOLWIND 1979 17A COSMOS-1129 1979 83A COSMOS—1081 1979 24A HAKUCHO 1979 14A SOYUZ-32 1979 18A COSMOS-1130 1979 84A COSMOS-1082 1979 24B HEAO-3 1979 82A SOYUZ-33 1979 29A COSMOS-1131 1979 84B C0SM0S-1083 1979 24C SOYUZ-34 1979 49A COSMOS-1132 1979 84 C COSM0S-1084 1979 24D SOYUZ-T 1979 103A COSMOS-1133 1979 84D 1 COSMOS-1085 1979 24E STATSIONAR-1 1979 35A COSMOS-1134 1979 84 E COSMOS-1086 1979 24F STATSIONAR—4 1979 62A COSMOS-1135 1979 84F C0SM0S-1087 1979 246 INTERCOSMOS-19 1979 20A STATSIONAR-5 1979 105A COSMOS—1088 1979 24H COSMOS-1136 1979 84G INTERCOSMOS-20 1979 96A ST AT S10NAR-T 1979 87A COSMOS—1089 COSMOS-1137 1979 84H 1979 26 A STP P78-1 1979 17A COSMOS-1138 1979 8 5A C0SM0S-109Q 1979 27A STP P78-2 1979 7 A C0SM0S-1091 1979 28A COSMOS-1139 1979 88 A COSMOS—109 2 1979 30A C0SM0S-1140 1979 89A M C0SM0S-1093 1979 32A COSMOS-1141 1979 90A COSMOS-1094 1979 33A COSMOS-1142 1979 92 A MAGSAT 1979 94A u C0SM0S-1095 1979 34A COSMOS-1143 1979 93 A METEOR-1 (29) 1979 5A UK-6 1979 47 A C0SM0S-1096 1979 36A COSMOS-1144 1979 97A METEOR-2 (4) 1979 21A CCSMOS-1097 19 79 37A COSMOS-1145 1979 99A METEOR-2 (5) 1979 95A COSMOS-1098 1979 40A COSMOS-1146 1979 100A MOLNYA-1 (43) 1979 31 A W COSMOS-1099 1979 41A COSMOS-1147 1979 1 02A MOLNYA-1 (44) 1979 70A COSMOS-11 00 1979 42 A COSMOS-1148 1979 1 06 A MOLNYA-1 (45) 1979 91A WESTAR-3 1979 72A C ountry Code name international Organization Perigee Period Frequencies Date Observations Spacecraft description num ber Site o f Apogee Inclination Transmitter p ow e r launching Cosmos-1070 1979-1-A USSR 11 Jan. 214 km 89.5 min Reconnaissance satellite. (PLE) 316 km 62.8° Recovered on 20 January 1979 Cosmos-1071 197 9 -2 -A USSR 13 Jan. 190 km 89.7 min High-resolution reconnaissance satellite. (PLE) 360 km 62.8° Recovered on 26 January 1979 Cosmos-1072 1979 -3-A USSR 16 Jan. 983 km 105.0 min Navigation satellite (PLE) 1030 km 83.0° 11th Molnya-3 19 7 9-4-A USSR 18 Jan. 474 km 5.9-6.2 GHz Carries apparatus for transmitting television programs (PLE) 40 806 km 62.8° (reception) and multichannel radiocommunications 3-axis stabilized satellite; mass: 1500 kg 3.6-3.9 GHz (transmission) 29th Meteor-1 19 7 9-5-A USSR 25 Jan. 628 km 97.4 min Meteorological satellite (PLE) 656 km 98.0° 3-axis stabilized cylindrical satellite; mass: 2200 kg; sun- oriented solar panels Cosmos-1073 1979-6-A USSR 30 Jan. 187 km 89.6 min Reconnaissance satellite. (PLE) 350 km 62.8° Recovered on 12 February 1979 SCATHA (STP P78-2) 19 7 9-7-A United States 30 Jan. 184 km 794.8 min 2241.5; 2244.5 MHz Spacecraft Charging AT High Altitudes. Carries 12 ex­ USAF 43 905 km 27.4° 5 W periments to identify and measure sources of electrical spin-stabilized cylindrical (ETR) charge build-up spacecraft; diameter: 1.70 m; 5765.0 MHz height: 1.80 m; mass: 343 kg 400 W 2250.5 MHz 3W 2222.5 MHz Cosmos-1074 19 7 9-8-A USSR 31 Jan. 203 km 88.8 min Decayed on 1 April 1979 256 km 51.6° Ayame 1979-9-A Japan 6 Feb. 193 km 604 min 31.65 GHz Experimental telecommunication satellite intended NSDA 34 411 km 24.1 ° 3.2 W for geostationary orbit. Ceased transmission on 9 Feb­ cylindrical satellite; diameter: (TSC) ruary during an attempt to move it into synchronous 1 m; height: 1.50 m; mass 4.075; 4.080 GHz orbit 260 kg 4.7 W 3.940 GHz 3.5 W 136.112 MHz 2 and 8 W 1 TELECOMMUNICATION JOURNAL - VOL. 47 - IVI1980 Country Code name International Organization Perigee Period Frequencies Date Observations Spacecraft description num ber Site o f Apogee Inclination Transmitter p ow e r launching Cosmos-1075 1979-10-A USSR 8 Feb. 475 km 94.6 min Space intercept program (PLE) 521 km 6 5.8 “ Cosmos-1076 1979-11-A USSR 13 Feb. 647 km 97.0 min Oceanographic satellite (PLE) 678 km 82.0° Cosmos-1077 1979-12-A USSR 14 Feb. 629 km 97.3 min (PLE) 651 km 81.2° SAGE 1979-13-A United States 18 Feb. 544 km 96.9 min Stratospheric Aerosol and Gas Experiment. Objectives: (W l) 655 km 57.9° to obtain global data on stratospheric aerosols and 3-axis stabilized spacecraft; ozone during at least one year. Carries a 4-spectral 6-sided prism shape; height: radiometer to measure solar intensity attenuation after 0.64 m; mass: 147 kg; 2 solar sunrise and before sunset in wavebands centred at panels 0.385, 0.45, 0.6 and 1.0 //m CORSA-B (Hakucho) 1979-14-A Japan 21 Feb. 545 km 96.0 min 136.725 MHz COsmic Radiation SAtellite. Objectives: cosmic and University of 577 km 29.9° 500 mW X-ray stellar observation.Two experiments cover the octagonal spacecraft; breadth: Tokyo 400.45 MHz ranges 0.1 to 2 keV and 1.5 to 30 keV 0.82 m; height: 0.46 m; gross (KSC) 100 mW mass: 96 kg; solar cells (data transmission) 148 MHz (reception of commands) Ekran-3 1979-15-A USSR 21 Feb. 35 780 km 1436 min 5.7-6.2 GHz Carries equipment for television transmission (BAI) 0.35° (reception) 3-axis stabilized satellite; mass: in geostati Dnary orbit 5 tonnes; solar cells at 53 ° E 3.4-3.9 GHz (transmission) Cosmos-1078 1979-16-A USSR 22 Feb. 180 km 89 min Reconnaissance satellite. (PLE) 306 km 72.9° Recovered on 2 March 1979 Solwind (STP P78-1) 1979-17-A United States 24 Feb. 560 km 96.3 min 2242,5; 2247.5 MHz Space Test Program. Carries gamma-ray spectrometer USAF 600 km 97.9° 10 W and six other experiments designed to gather data on mass. 1331 kg; similar to OSO-7 (WTR) 2252.5 MHz solar wind, solar flares, electron build-up around the (1971-83-A) 2 W Earth's polar regions and the distribution of aerosols (telemetry) and ozone in the atmosphere Soyuz-32 1979-18-A USSR 25 Feb. 244 km 89.6 min Two-man spacecraft: V. Lyakhov, flight commander; (BAI) 283 km 51.6° V. Ryumin, flight engineer. Docked with S alyut-6 (1977 3-part spacecraft: 2 spherical 97-A) on 26 February. On 1 March Soyuz-32 was used habitable modules (orbital com­ as a locomotive to transfer Salyut-6 into a higher orbit partment and command module) (308/328 km).
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