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At an orbital height of 500 km, find the orbital period of the satellite.
 
Given:
 
h = 500 km
 
R = 6371\ km
 
v = 7.616 kms^{-1}
 
Formula:
 
T=iπi+iiii+i
 
On substituting the given values, we get
 
T=i×227×i+ii
 
The orbital period of the satellite is  minutes.
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