A satellite is in an inclined (i = 105 deg), eccentric orbit with pergiee altitude of 350 km, an apogee altitude of 15850 km. The argument of perigee is 90 deg. 30 days later, the new argument of perigee value in degrees, is what?
A satellite is in an inclined (i = 105 deg), eccentric orbit with pergiee altitude of 350 km, an apogee altitude of 15850 km. The argument of perigee is 90 deg. 30 days later, the new argument of perigee value in degrees, is what?
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Transcribed Image Text:A satellite is in an inclined (i = 105 deg), eccentric orbit with pergiee altitude of 350 km, an apogee altitude of 15850 km. The argument of perigee is 90 deg. 30 days later, the new argument of perigee value in
degrees, is what?
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