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[" If due to air drag,the orbital radius...

[" If due to air drag,the orbital radius of "],[" satellite decreases from "R" to "R-Delta R,Delta R<<],[R," then the expression for change in orbital "],[" velocity "Delta v" is "],[" [mass of earth "M]:-],[" (Dass of earth "M]:-],[" (D) "(Delta R)/(2)sqrt((GM)/(R^(3)))],[" (8) "Delta R sqrt((GM)/(R^(3)))],[" (8) "Delta R sqrt((GM)/(R^(3)))],[" - LambdaR "-Delta B/(GM)/(R^(3))]

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