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... -mi) apogee, 162.5-km (101-mi) perigee, 88.7-min period, and 96.9° inclination and reentered March 13, 1974. The second entered orbit with a 505.3-km (314-mi) apogee, 487.6-km (303-mi) perigee, 94.5-min period, and 96.3° inclination. Orbital parameters for the third satellite were 1458.1-km (906-mi) apogee, 1417.8 ... -mi) apogee, 217-km (134.8-mi) perigee, 89.6-min period, and 72,2° inclination. The satellite reentered Nov. 22. ''( GSFC SSR, 11/30/73; SBD, 11/13/73, 66 ...

... had discovered only two other near-earth asteroids with orbital inclinations higher than 1985-PA. Helin said the asteroid's inclination suggested it could have had a close encounter with Mars and been knocked into the steeply inclined orbit. At discovery the asteroid was moderately bright-measuring at 16.5 magnitude-and reddish ...

... maneuvers '' are those that change the orientation of the orbit, thus altering the inclination. To change the inclination only, the spacecraft’s thrusters must be fired at either the ascending or descending ... at any other point in a generic orbit alters both the inclination and the ascending node. GEO satellites must maintain their inclination to minimize their North-South drift. Out-of-plane maneuvers ...

... : apogee, 545 mi ''(877 km)'' ; perigee, 324 mi ''(521 km)'' ; period, 98.8 min and inclination 59A°. Primary NASA objective was to place satel­lite in planned orbit and provide tracking ... ''(524-mi)'' apogee, 271-km ''(168-mi)'' perigee, 95.7-min period, and 70.9° inclination. Cosmos CCV entered orbit with 292-km ''(181-mi)'' apogee, 197-km ''(122-mi)'' perigee, 89.3-min period, and 65.6° inclination. Cosmos CCV reentered March 13. Cosmos CCIV reentered March 2, 1969. ''(AP, NYT, 3/7 ...

... -km)'' apogee, 114-mi ''(183.5-km)'' perigee, 90.2-min period, and 83.1° inclination and reentered April 10. Second entered orbit with 326-mi ''(524.6-km)'' apogee, 299-mi ''(448.2-km)'' perigee, 94.6-min period, and 31.6° inclination. ''(Pres Rpt 68; SBD, 3/18/68, 91)'' U.S.S.R. successfully launched Cosmos ... : apogee, 640 km ''(398 mi)''; perigee, 598 km ''(372 mi)'' ; period, 97.1 min; and inclination, 81.2°. ''(GSFC SSR, 3/15/68; AP, NYT, 3/20/68, 10)'' Spacecraft for ...

... : apogee, 1,837 km. (1,141 mi.) ; perigee, 273 km. (170 mi.) ; period, 106 min.; inclination, 56°. It was reported that the scientific apparatus onboard was functioning normally. ''(Krasnaya Zvezda, 3 ... II had 308 mi. (496.7 km.) apogee, 108 mi. (174.4 km. perigee. 65° inclination; COSMOS LVII had 317 mi. (511.3 km.) apogee, 107 mi. ( 172.6 km.) perigee, and 65° inclination. According to NASA Goddard Space Flight Center 's Satellite Situation Report, 51 pieces of COSMOS ...

... ,942.5 km.) ; perigee, 66,583 mi. (107,198.6 km.) ; period, 6,713 min,; inclination, 34.6°; VELA 6564-10: apogee, 75,761 mi. (121,975.2 km,) ; perigee, 63,224 mi. ( 101,790.6 km,) ; period, 6,716 min,; inclination, 34.8°; ORS 111-1: apogee, 69,640 mi. (112,120.4 km,) ; perigee, 123 mi. (198 km,) ; period, 6,715 min,; inclination, 34.3°. Expected to operate six months, the Vela Hotel satellites were part of DOD ...

... mi. (1,511 km.) ; perigee, 250 mi. (403.1 km.) ; period, one hour 45 min.; inclination, 87°. Planned orbit had been somewhat lower: 575-mi. (925-km.) apogee, 207-mi. (333,3-km,) perigee, one-hour 37-min. period, and 86° inclination. Most of the 20 onboard experiments were not expected to be affected by the malfunction ... ,000 km. (24,800 mi.) ; perigee, 500 km. (310 mi.) ; period, 11 hrs, 59 min.; inclination, 65°, Tass said: "With the launching of the second MOLNIYA I satellite, verification will begin ...

... : apogee, 1,768 km. (1,098 mi,) ; perigee, 525 km. (326 mi,) ; period, 108 min.; inclination, 34.65° (compared with planned 2,154-km, 1,562-mi. apogee, 553-km, 331-mi, perigee, 53° inclination). The 88-lb, satellite, comparable to the U.S. Vanguard Program Vanguard , carried a radio ... ,100 km. (1,304 mi,) ; perigee, 220 km. (136.6 mi,) ; period, 108.3 min,; inclination to equator, 49°. Onboard equipment was operating normally. ''(Pravda, 11/27/65, 1, ATSS-T ...

... km (260-mi) lower than nominal; 584km (363-mi) perigee; 104-min period; and 40ø inclination. Reason for low apogee had not yet been determined. Designed to reflect laser beams fired ... (214-mi) apogee; 210-km (130-mi) perigee; 89.8-min period; and 72.9' inclination. All equipment functioned normally. Satellite reentered Feb. 16. ''(UPI, NYT, 2/9/67; Goddard Space ... photography. Orbital parameters: apolune, 1,145 mi (1,847 km); perilune, 34 mi (55 km); inclination, 20.93ø; and period, 3 hrs 29 min. Spacecraft performed 357 attitude changes, responded to ...

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