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Calculate the speed with which a satellite moves if it is at a height of \(36,000\ km\) from the Earth’s surface and has an orbital period of \(24\ hr\).
 
[HINT: Take \(R = 6370\ km\) and convert \(hour\) into \(seconds\) before doing calculation.]
 
Given:
 
\(h\) \(=\) \(36000\ km\)
 
\(t\) \(=\) \(24\ h\)
 
On converting \(hr\) to \(s\), we get \(s\).
 
Formula:
 
T=iπi+iiii+i
 
(or)
 
T=iπi+ii
 
On substituting the given values, we get
 
v=i×3.14×i+ii
 
Orbital velocity of a satellite \(=\)  \(kms^{-1}\) [NOTE: Enter up to two decimal places for answers.]
 
On calculating speed, we get
 
Speed=ii
 
Speed \(=\)  \(kmh^{-1}\) [NOTE: Enter up to three decimal places for answers.]