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... (929-mi) apogee, 1450-km (901-mi) perigee, 115.3-min period, and 74.0° inclination. Cosmos 589-4489-km (925.2-mi) apogee, 1417-km (880.5-mi) peri-gee ... ) apogee, 1400-km (869.9-mi) peri-gee, 114.7-min period, and 73.9° inclination. Kenneth W. Gatland of the British Interplanetary Society later said in a Christian Science Monitor ... -mi) apogee, 205-km (127.4-mi) perigee, 89.2-min period, and 65.4° inclination. The satellite reentered Oct. 9. Cosmos 596 was the first of seven Soviet satellites launched ...

... .6-mi) apogee, 1469-km (912.8-mi) perigee, 116.2-min period, and 74° inclination; Cosmos CCCXXXVIII, 1517-km (942.6-mi) apogee, 1472-km (914.7-mi) perigee, 115 ... .4-m ) apogee, 1312-km (815.2-mi) perigee, 113.5-min period, and 74° inclination; and Cosmos CCCXLIII, 1468-km (912.2-min) apogee, 1379km (856.9-mi) perigee, 114.2-min period, and 74° inclination. All systems were functioning satisfactorily. ''( Goddard Space Flight Center GSFC SSR, 4/30/70,; AP ...

... .7-mi) apogee, 1317-km (818.3-mi) perigee, 113.8-min period, and 74° inclination. Others entered following orbits: Cosmos 412, 1536-km (954.4-mi) apogee, 1482-km (920 ... (937-mi) apogee, 1476-km (917.2-mi) perigee, 115.7-min period, and 74° inclination; Cosmos 414, 1495-km (928.9-mi) apogee, 1428-km (887.3-mi) perigee, 1151 ... .3-mi) apogee, 1401-km (870.5-mi) perigee, 114.8-min period, and 74° inclination. ''( Goddard Space Flight Center GSFC SSR, 5/31/71; SBD, 5/11/71, 53)'' Nonexplosive ...

... .3-mi) apogee, 1323-km (822.1-mi) perigee, 114.1-min period, and 74° inclination. Cosmos 445, 1513-km (940.1-mi) apogee, 1352-km (840.1-mi) perigee, 114 ... (942-mi) apogee, 1412-km (877.4-mi) perigee, 115.1-min period, and 74° inclination. Cosmos 448, 1518-km (943.2-mi) apogee, 1442-km (896-mi) perigee, 115.5-min period, and 74° inclination. Cosmos 449, 1542-km (958.2-mi) apogee, 1485-km (922.7-mi) perigee, 116 ...

... (930.8-mi) apogee, 1384- km (860-mi) perigee, 114.6-nun period, and 74° inclination. Cosmos 507 entered orbit with 1497-km (930.2-mi) apogee, 1414-km (878.6 ... (939.5-mi) apogee, 1496- km (929.6-mi) perigee, 116-min period, and 74° inclination. Cosmos 511 entered orbit with 1547-km (961.3-mi) apogee, 1496-km (929.6-mi) perigee, 116.4-min period, and 74° inclination. ''( Goddard Space Flight Center GSFC SSR, 7/31/72; Sov Aero, 7/24/72, 30 ...

... -mi) apogee, 1368- km (850.1-mi) perigee, 114.1-min period, and 74.0° inclination. Cosmos 529 entered orbit with 1469-km (912.8-mi) apogee, 1404- km (872.4-mi) perigee, 114.5-min period, and 74.0° inclination. Cosmos 530 entered orbit with 1469-km (912.8-mi) apogee, 1335-km (829.5 ... -mi) apogee, 1386-km (861.2-mi) perigee, 114.3-min period, and 74.0° inclination. Last U.S.S.R. eight-payload launch had been on July 20. Western specialists ...

... -mi) apogee, 1397-km (868.1-mi) perigee, 114.6-min period, and 74.0° inclination. Cosmos 565, with a 1493-km (927.7-mi) apogee, 1448-km (899.7-mi) perigee, 115.3-min period, and 74.0° inclination. Cosmos 566, with a 1484-km (922.1-mi) apogee, 1435-km (891.7-mi ... -mi) apogee, 1322-km (821.5-mi) perigee, 113.7-min period, and 74.0° inclination. ''( GSFC SSR, 6/30/73; SBD, 6/12/73, 233; Shabad, NYT, 6/10/73 ...

... -mi) apogee, 1336-km (830.2-mi) perigee, 114.0-min period, and 74.0° inclination. Cosmos 618-1488-km (924.6-mi) apogee, 1445-km (897.9 mi) perigee, 115.2-min period, and 74.0° inclination. Cosmos 619-1490-km (925.8-mi) apogee, 1424-km (884.8-mi) perigee, 115 ... -mi) apogee, 1353-km (840.7-mi) perigee, 114.2-min period, and 74.0° inclination. The Western press reported that the satellite system would operate in support of Soviet naval ...

... perigee, 114.5-min period, and 74.0° inclination. Cosmos 678-1533-km apogee, 1466-km perigee, 116.0-min period, 74.0° inclination. Cosmos 679-1511-km apogee, 1466-km perigee, 115.8-min period, 74.0° inclination. Cosmos 680-1492-km apogee, 1466-km perigee ... -km perigee, 114.9-min period, 74.0° inclination. Cosmos 684-1467-km apogee, 1416-km perigee, 114.7-4n period, 74.0° inclination. The U.S. press speculated that the satellites ...

... )'' apogee 90.8- mi ''(146.2-km)'' perigee, 87.7-min period, and 28.6° inclination. Second transtage burn moved stage and payload into elliptical transfer orbit with 22,241-mi ... ,777.7-km)'' apogee, 115-mi ''(185-km)'' perigee, 630.8-min period, and 26A° inclination, where satellite would investigate radiation in Van Allen belts. Third transtage burn put satellite dispenser ... , 22,220-mi ''(35,771.9-km)'' perigee, 1,435.8-min period, and 3° inclination. OV 11-5, synchronous-altitude research satellite equipped with 10 sensors to investigate radiation, entered ...

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