Answer on Question #54957, Physics / Astronomy | Astrophysics
We need draw the artificial satellite is at perigee at A (the point in its orbit nearest the Earth's centre E) and at apogee at A' (when it is farthest from the Earth's centre):

The size of the major axis AA' of the ellipse is given by:
AA′=4023+2×6372+660=17427km
So that the semi-major axis a1 is of length 8713⋅5km . The period of revolution is T1=134 minutes. For the Earth orbit:
a=149.5×106kmT=365.25×24×60=5.2596×105 minutes.
Letting M and m be the masses of Sun and Earth respectively, we have, using equation:
Mm=(5.2596×105134)2(8713.5149.5×106)3=327800
Answer: m/M=327800
http://www.AssignmentExpert.com/
Comments