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Table of Artificial Satellites Launched in 1971

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Table of Artificial Satellites Launched in 1971 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 A COSMOS-428 1971 57A E 0 COSMOS-429 1971 61A COSMGS-430 1971 62A COSMOS-431 1971 65A APOLLO-14 1971 8A COSMOS-432 1971 66A EOLE 1971 71A OAR-901 1971 67C APOLLO-15 1971 63A COSMOS-433 1971 68A EXPLORER-43 1971 19A CAR-907 1971 67D APOLLO-15 CSUB•SAT 3 1971 63D COSMOS-434 1971 69A EXPLORER-44 1971 58A OREOL-1 1971 119A ARIEL-4 1971 109A COSMOS-435 1971 72A EXPLORER-45 1971 96A OSO- 7 1971 83A COSMOS-436 1971 74A OV1-20 1971 67A C COSMOS-437 1971 75A 0V1-21 1971 67B COSMOS-438 1971 77A 1 1971 COSMOS-439 78A P C0SM0S-44Q 1971 79A CANNON BALL-2 1971 67C COSMOS-441 1971 81A COSMOS-390 1971 1A COSMOS-442 1971 84A IMEWS-2 1971 39 COSMOS-391 1971 2A COSMOS-443 1971 85A IMP-I 1971 19A COSMOS-392 1971 4A COSMOS-444 1971 86A INTELSAT-IV-F2 1971 6A PROSPERO 1971 93A COSMOS-393 1971 7A COSMOS-445 1971 86B INTELSAT-XV-F3 1971 116A COSMOS-394 1971 10A COSMOS-446 1971 86C INTERCOSMOS-5 1971 104A COSMOS-395 1971 13A COSMOS-447 1971 86D ISIS-2 1971 24A s COSMOS-396 1971 14A COSMOS-448 1971 86E ITOS-B 1971 91A TO 1971 91D COSMOS-397 1971 15A COSMOS-449 1971 86F COSMOS-398 1971 16A C0SM0S-45Q 1971 86G 1971 COSMOS-399 1971 17A COSMOS-451 86H L SALYUT- 1 1971 32A COSMOS-452 1971 88A COSM05-400 1971 20 A SAMOS-81 1971 5 C0SM0S-4Q1 1971 23A COSMOS-453 1971 90 A SAMOS-82 1971 COSMOS-454 1971 33A COSM05-402 1971 25A 94A SAMOS-83 1971 56 COSMOS-455 1971 97A COSMOS-403 1971 26A 1971 SAMOS-84 1971 70A COSMOS-456 1971 98A LUNA-18 73A C0SM0S-404 1971 27A LUNA-19 1971 82A SAMOS-85 1971 92 A C0SM0S-4Q5 1971 28A COSMOS-457 1971 99A 1971 SAN-MARCO-3 1971 36A COSMGS-406 1971 29A COSMOS-458 101A SHINSEI 1971 COSMOS-459 1971 M 80A CQSMOS-407 1971 35A 102A SOLRAD-IO 1971 COSMOS-460 1971 58A COSMOS-4O8 1971 37A 103A SOYUZ-IO 1971 34A COSMOS-409 1971 38A COSMOS-461 1971 005A SOYUZ-11 1971 53A COSMOS-462 1971 106A COSMOS-410 1971 <+0A SSS-A 1971 96A COSMOS-411 1971 41A COSMOS-463 1971 107A MARINER- 9 1971 51A STP 1971 89A COSMOS-412 1971 41B COSMOS-464 1971 108A MARS-2 1971 45A COSMOS-465 1971 111A COSMOS-413 1971 41C MARS-3 1971 49A T COSMOS-414 1971 41D COSMOS-466 1971 112A METEOR- 7 1971 3A COSMOS-415 1971 41E COSMOS-467 1971 113A METEOR- fi 1971 31A COSMOS-416 1971 41F COSMOS-468 1971 114A METEOR- 9 1971 59A COSMOS-417 1971 41G COSMOS-469 1971 117A METEOR-IO 1971 120A COSMOS-418 1971 41H COSMOS-470 1971 118A MOLNYA-1R 1971 64A TANSEI 1971 11A COSMOS-419 1971 42A MOLNYA-1S 1971 115A TETR-3 1971 83B COSMOS-420 1971 43A 0 M0LNYA-2A 1971 100A TOURNESOL 1971 30 A COSMOS-421 1971 44A MUSKET BALL 1971 67D COSMOS-422 1971 46A N U COSMOS-423 1971 47 A COSMOS-424 1971 48A COSMOS-425 1971 50A D-2A 1971 30 A COSMOS-426 1971 52A DSCS-1 1971 95A COSMOS-427 1971 55A DSCS-2 1971 95B NATO-2 1971 9A UK-4 1971 109A Country Code nam e International Organization Date Perigee Period Frequencies Observations Spacecraft number Site o f Apogee Inclination Transmitter description launching power Cosmos-390 1971-1-A USSR 12 Jan. 208 km 89.3 min Carried scientific apparatus, radio system for precise (BAI) 296 km 65° measurements of orbital elements, and radiotelemetry system. Reconnaissance/surveillance mission. Decayed on 25 January 1971 Cosmos-391 1971-2-A USSR 14 Jan. 277 km 95.4 min Carried scientific apparatus, radio system for precise (PLE) 828 km 71° measurements of orbital elements, and radiotelemetry system . Decayed on 21 February 1972 Meteor-7 1971-3-A USSR 20 Jan. 630 km 97.6 min Carries meteorological apparatus, radio system for (PLE) 679 km 81.2° precise measurements of orbital elements, and radio­ telemetry system Cosmos-392 1971-4-A USSR 21 Jan. 207 km 89.4 min 19.995 MHz Carried scientific apparatus, radio system for precise (BAI) 300 km 65° measurements of orbital elements, and radiotelemetry system. Reconnaissance/surveillance mission. Decayed on 2 February 1971 Samos-81 1971-5-A U nited 21 Jan. 131 km 89.6 min Reconnaissance/surveillance mission. States 382 km 110.8° (W TR) Decayed on 9 February 1971 Intelsat-IV F2 1971-6-A International 26 Jan. 35 740 km 1450.2 min 5950; 5990; 6030; 6070; 6110; INTELSAT commercial telecommunication satellite. INTELSAT 36 382 km 0.6° 6150; 6200; 6240; 6280; 6320; 3000 to 9000 telephone circuits or 12television channels. weight: 720 kg; cylindrical (ETR) 6360; 6400 MHz In geostationary orbit above the Atlantic Ocean at satellite; height: 5.28 m; (reception) 335.5° E longitude diameter: 2.39 m; solar cells 3725; 3765; 3805; 3845; 3885; 3925; 3975; 4015; 4055; 4095; 4135; 4175 MHz (transmission) Cosmos-393 1971-7-A USSR 26 Jan. 283 km 92.2 min Carried scientific apparatus, radio system for precise 512 km 71° measurements of orbital elements, and radio telemetry system . Decayed on 16 June 1971 1 TELECOMMUNICATION JOURNAL - VOL. 39 - IV/1972 C ountry Code name International Organization Date Perigee Period Frequencies Observations Spacecraft num ber Site o f Apogee Inclination Transmitter description launching power Apollo-14 1971-8-A United 31 Jan. baryce ntric orbit 5765 MHz Three-man spacecraft: astronauts Alan B. Shepard Jr. States 450 W peak (commander), Stuart A. Roosa (command module pilot), w eight: 44 676 kg; command (radar tracking beacon) Edgar D. Mitchell (lunar module pilot). Third lunar module; service module; lunar landing (Fra Mauro); 44 kg of lunar material was brought module; diameter: 3.90 to 2272.5 ; 2287.5 MHz back. The command module splashed down on 9 Feb­ 6.60 m; tota l height: 29 m 20 W ruary 1971 (data transmitted on command from the command module) 2282.5 MHz 20 W (data transmitted from the lunar module) N a t o-2 1971-9-A International 3 Feb. 34 429 km 23 h 23 min X band Communication satellite NATO 35 860 km 28° w eight: 129 kg (ETR) Cosmos-394 1971-10-A USSR 9 Feb. 574 km 96.5 min Carries scientific apparatus, radio system for precise 619 km measurements of orbital elements, and radiotelemetry length: 4 m; diameter: 2 m system. Manoeuvres near Cosmos-397 Tansei 1971-11-A Japan 16 Feb. 989 km 106 min 136.6952 MHz Japanese technological test satellite. Estimated trans­ 1109 km 30° 90 m W m itter life is one week 26-sided body; diam eter across (tracking beacon— continuous flat sides: 0.712 m; chemical transmission) batteries; reflectors for optical detection 400.4971 MHz 45 m W (with real time telemetry) 4 satellites: weight: 0.730 kg; 1971-12-A(?) United 17 Feb. 763 km 100.86 min spheroid; States 833 km 98.8° diam eter: 26 m (W TR) w eight: 0.730 kg; 1971 -12-B(?) United 17 Feb. 765 km 100.89 min spheroid; States 834 km 98.8° diam eter: 26 m (WTR) Study of atmospheric drag weight: 0.730 kg; 1971-12-C(?) United 17 Feb. 773 km 100.95 min spheroid; States 832 km 98.8° diam eter: 26 m (W TR) w eight: 150 kg; 1971-12-D(?) United 17 Feb. 779 km 100.96 min spacecraft States 827 km 98.8° (W TR) 2 Cosmos-395 1971-13-A USSR 18 Feb. 534 km 95.4 min Carries scientific apparatus* radio system for precise (PLE) 570 km 74° measurements of orbital elements, and radiotelemetry system Cosmos-396 1971-14-A USSR 18 Feb. 212 km 89.4 min Carried scientific apparatus, radio system for precise 310 km 65.4° measurements of orbital elements, and radiotelemetry system. Soyuz-type satellite. The orbital compartment re-entered the atmosphere on 8 March 1971. The recoverable part returned to the earth on 3 March 1971 Cosmos-397 1971-15-A USSR 25 Feb. 593 km 114.7 min Carried scientific apparatus, radio system for precise 2317 km 65.8° measurements of orbital elements, and radiotelemetry system. Manoeuvrable satellite. Disintegrated in space Cosmos-398 1971-16-A USSR 26 Feb. 196 km 88.9 min Carries scientific apparatus, radio system for precise 276 km 51.63° measurements of orbital elements, and radiotelemetry system.
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