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... entered lunar orbit with 140-km (87-mi) altitude, 122-min period, and 40° 35' inclination. Tass said Oct. 19 that all systems were operating normally and spacecraft was conducting geophysical ... .4-mi) apogee, 619-km (384.6-mi) perigee, 133-min period, and 31.2° inclination. Purpose of mission was to study cosmic rays and solar electric waves for one year ... .3-mi) apogee, 207-km (128.6-mi) perigee, 89.2-min period, and 65° inclination. Satellite reentered Oct. 10. ''( GSFC SSR, 9/30/71; 10/31/71; SBD, 10/1 ...

... -mi) apogee, 199-km (123.7-mi) perigee, 89.7-min period, and 72.8° inclination. Satellite reentered Oct. 12. ''( Goddard Space Flight Center GSFC SSR, 9/30/71; 10/31 ... ) apogee, 329.1-km (204.5-mi) perigee, 93.6-min period, and 33.1° inclination. Primary mission objective was to obtain high-resolution data from solar corona in particular spectral ... .8-mi) apogee, 391-km (243-mi) perigee, 94.3-min period, and 33,0° inclination. Primary objective of 45-lb (20.4-kg) secondary payload was to test Manned Space ...

... -mi) apogee, 260-km (161.6-mi) perigee, 92.7-min period, and 48.4° inclination. Objective of mission was "to continue joint studies of the sun's ultra- violet and ... .0-mi) apogee, 271-km (168.4-mi) perigee, 95.2-min period, and 71° inclination. Meteor 12 weather satellite was launched from Plesetsk to obtain "meteorological information necessary for swift ... ." Orbital parameters: 904-km (561.7-mi) apogee, 888-km (551.8) perigee, 81.2° inclination, and 102.8-min period. ''( Goddard Space Flight Center GSFC SSR, 6/30/72, 7 ...

... (546-mi)'' apogee, 824-km (512-mi) perigee, 101.5-min period, and 98.6° inclination. ''(Pres Rpt 73; SBD, 11/16/70, 70)'' NASA's M2-F3 lifting body completed ... of 36 470 km (22 661.4 mi); perigee, 188.9 km (117.4 mi); inclination, 26.9°. After checkout and reorientation of spacecraft, apogee kick motor on board Anik 1 ... ) apogee, 35 822-km (22 258.8-mi) perigee, 1455-min period, and 0.4° inclination and drifting to final operating position in synchronous equatorial orbit off west coast of South ...

... .9-mi) apolune, 1123-km (697.8-mi) perilune, 241-min period, and 61.3° inclination, On June 18 the lunar insertion motor was jettisoned and the hydrazine-fueled velocity-control ... .5-mi) apolune, 1052-km (653.7- mi) perilune, 22L2-min period, and 38.7° inclination. On June 20 a 37-m (120-ft) dipole antenna was extended by ground control ... -mi) apogee, 199-km (123.7- mi) perigee, 89.4-min period, and 51.8° inclination. The satellite reentered June 23. ''( GSFC SSR, 6/30/73; SBD, 6/13/73, 242 ...

... -mi) apogee, 128.8-km (80-mi) perigee, 89.8-min period, and 110.5° inclination. The satellite reentered Oct. 29. ''(Pres Rpt 74; Wilson, W Post, 10/16/73, A7 ... .3-mi) apogee, 180-km (111.8-mi) perigee, 88.6-min period, and 513° inclination. Soviet news agency Tass announced the objectives of the two-day mission were to test ... .4-mi) apogee, 326-km (202.6-mi) perigee, 91-min period, and 51.6° inclination. The cosmonauts also made spectrographs of natural formations of the earth's surface. They were ...

... 799.9-km (22 245-mi) perigee, 24-hr 5-min period, and 2.0° inclination. Dscs F-4 entered orbit with a 36 137.8-km (22 455-mi) apogee ... 944.7-km (22 335-mi) perigee, 24-hr 9-min period, and 2.0° inclination. On Dec. 19 the press reported Air Force officials as saying that the satellites-part ... -mi) apogee, 269-km (167.2-mi) perigee, 95.6-min period, and 71.0° inclination. ''(cSFC SSR, 12/31/73)'' NASA announced the selection of Grumman Aerospace Corp. for negotiation ...

... orbit with 252-km apogee, 213-km perigee, 89.2-min period, and 51.6° inclination. Tass announced the purpose of the mission was to improve the station's design, onboard ... with a 338-km apogee, 201-km perigee, 89.9-min period, and 51.5° inclination. Maj. Gen. Vladimir A. Shatalov , chief of cosmonaut training, said during a 4 July Tass ... with a 277-km apogee, 255-km perigee, 89.7-min period, and 51.6° inclination. All spacecraft systems were success-fully checked out and the crew was reported to be ...

... orbit with 246-km apogee, 183-km perigee, 88.7-min period, and 51.5° inclination, where the "automatic station" was separated and launched on a near-to-planned trajectory to ... a, lunar orbit with 104-km apogee, 94-km perigee, 117-min period, and 138° inclination. On 4 and 5 Nov. the orbit was changed to 105-km apogee and 17 ... orbit with 904-km apogee, 842-km perigee, 102.4-min period, and 81.2° inclination. Tass reported that the spacecraft carried meteorological equipment to photograph cloud formations and snow cover ...

... with a 279-km apogee, 152-km perigee, 88.8-min period, and 96.7° inclination and reentered 19 March 1975. The second entered orbit with a 542-km apogee, 540-km perigee, 95.3-min period, and 96.1° inclination. The third entered orbit with a 3711-km apogee, 147-km perigee, 125.4-min period, and 97.0° inclination; it reentered 26 May 1975. ''(Pres Rpt 74; AFSC PAov, interview, 23 March 76; AFSC ...

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