find the value of g due to the earth at satellite. the radius of the satellite is 48700km.
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Answer:
For a satellite of mass m moving with a velocity v in a circular orbit of radius r around the earth of mass M, we have,
r
mv
2
=
r
2
GMm
or v=
r
GM
But v=
T
2πr
.
Thus
T
2πr
=
r
GM
or T∝r
2
3
∴
T
1
T
2
=(
r
1
r
2
)
2
3
2
=6400 km and r
1
=36000 km. For a geostationary satellite T
1
=24 h. Using these values in (1), we have get,
T
2
=24×( 36064)
23
=1.8 hours.
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