If an earth satellite is put in orbit at a height where resistance due to the atomosphere cannot be neglected, how will the motion of a satellite be affected ?

If an earth satellite is put in orbit at a height where resistance due

1.	If an earth satellite is put in orbit at a height where resistance due to the atomosphere cannot be neglected, how will the motion of a satellite be affected ?
Answer» <html><body><p></p>Solution :For a satellite, moving in a circular <a href="https://interviewquestions.tuteehub.com/tag/orbit-1138163" style="font-weight:bold;" target="_blank" title="Click to know more about ORBIT">ORBIT</a> of <a href="https://interviewquestions.tuteehub.com/tag/radius-1176229" style="font-weight:bold;" target="_blank" title="Click to know more about RADIUS">RADIUS</a> r orbital velocity `V_0=sqrt((GM)/r)<a href="https://interviewquestions.tuteehub.com/tag/therefore-706901" style="font-weight:bold;" target="_blank" title="Click to know more about THEREFORE">THEREFORE</a> Its K.E.=1/2mV_0^2=^1//_2m(GM)/r=^1//_2(<a href="https://interviewquestions.tuteehub.com/tag/gmm-2090431" style="font-weight:bold;" target="_blank" title="Click to know more about GMM">GMM</a>)/(2.r)and it's ` PE(GMm)/rxxr/(GMm)=^1//_2`</body></html>

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If an earth satellite is put in orbit at a height where resistance due to the atomosphere cannot be neglected, how will the motion of a satellite be affected ?

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