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Displaying 71—80 of 1000 matches for query "Inclination" retrieved in 0.001 sec with these stats:

  • "inclin" found 1719 times in 1371 documents



... .3-km)'' apogee, 425-mi ''(683-km)'' perigee, 117.9-min period, and 80.6° inclination. The 20.5-1b, 12-ft-dia inflatable sphere was covered with aluminum foil to ... ,530-km)'' apogee, 424-mi ''(677-km)'' perigee, 118.3-min period, and 80.6° inclination. Satellite's primary purpose was to measure directly down-flux of charged particles into atmos ...
... .6-mi)'' apogee, 590-km ''(366.6-mi)'' perigee, 96.8-min period, and 56° inclination. Cosmos CCXXXVII entered orbit with 323-km ''(200.7-mi)'' apogee, 199-km ''(123.6-mi)'' perigee, 89.7-min period, and 65.4° inclination and reentered Sept. 4. ''(csFC SSR, 8/31/68; 9/15/68)'' NASA issued Apollo ...
... -km)'' ap­ogee, 111-mi ''(178.6-km)'' perigee, 90.1-min period, and 83° inclination and reentered Oct. 8. Second satellite entered orbit with 318-mi ''(511.8-km)'' apogee, 312-mi ''(502.1-km)'' perigee, 94.7-min period, and 83.2° inclination. ''(Pres Rpt 68)'' Nike-Cajun sounding rocket launched by NASA from Churchill Research Range carried ...
... -km)'' apogee, 300- mi ''(482.8-km)'' perigee, 94.5-min period, and 74.9° inclination. ''(Pres Rpt 68)'' U.S.S.R. successfully launched Molniya 1-10 to relay telephone ... ''(24,630.5 mi)'' ; perigee; 429 km ''(266.6 mi)'' ; period, 711.9 min; and inclination, 64.8°. ''(UPI, W Star, 10/7/68, A9; AP, NYT, 10/8/68, 2 ...
... .1-mi)'' apogee, 735-km ''(467.8-mi)'' perigee, 100.6-min period, and 74° inclination. Cosmos CCLI entered orbit with 226-km ''(140.4-mi)'' apogee, 170 km ''(105.6-mi)'' perigee, 88.3-min pe­riod, and 64.7° inclination and reentered Nov. 18. Both satellites func­tioned normally. ''(GSFC SSR, 10/31/68; 11 ...
... au, or 69.71 million mi ''(112.19 million km)'' period, 297.55 days; and inclination 0.09°. Test and Training Satellite Tetr II ''(TETR-B)'' carried pickaback on 2nd stage ... -km)'' apogee, 231.3-mi ''(373-km)'' perigee, 97.9-min period, and 32.8° inclination. S-band transponder was operating properly. Tetr II was follow-on Tetr I ''(formerly desig ...
... -km)'' apogee, 109-mi ''(175.4-km)'' perigee, 88.6-min period, and 81.0° inclination and reentered Dec. 28. Second satellite entered orbit with 916-mi ''(1,474.1-km)'' apogee, 862-mi ''(1,387.2-km)'' perigee, 114.4-min period, and 80.3° inclination. ''(Pres Rpt 68)'' Two Nike-Cajun sounding rockets launched by NASA from Churchill Re­search ...
... -km)'' apogee, 161.9-mi ''(260.5-km)'' perigee, 642.9-min period, and 28A° inclination. All sys­tems were functioning normally. On Dec. 20 apogee motor was fired to kick ... -mi ''(35,933A-km)'' apogee, 21,8334- mi ''(33,137.5-km)'' perigee, 0.79° inclination, and 3.25° per day east­ward orbital drift. Intelsat-III F-2, first successful ...
... -mi.) apogee, 405-km. (252-mi.) perigee, 2-hr., 48 min. period, and 60.86¦ inclination to the equator. ELECTRON IV was orbiting at 66,235-km. (41,158-mi.) apogee, 459-km. (285-mi.) perigee, 21-hr., 54-min. period, and 60.86¦ inclination to the equator- ''(Tass, Izvestia, 7/12/64, 1, ATSS-T Trans.; AP, Wash. Eve ...
... satellite was orbiting with 578-mi. apogee, 252-mi. perigee, 98-min. period, and 81Ý inclination to the equator. NIMBUS I , unlike the Tiros meteorological satellites, was earth-oriented and stabilized ... -km. (534-mi.) apogee, 618-km. ''(384-mi.)'' perigee, 99.5-min. period, and 65° inclination to the equator. The satellite was said to be carrying on the Cosmos program announced ...

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