Question

Energy require to take satallite to height h above surfave is e1 and ke require for the satallite on orbit is e2 the value of h for which e1=e2 is

Answer 1

h = 3200 km.

You can refer the answer here:

https://www.entrance360.com/engineering/question-help-me-solve-this-the-energy-required-to-take-a-satellite-to-a-height-39h39-above-earth-surface-radius-of-the-earth-64-x-103km-is-e1-and-kinetic-energy-required-for-satellite-to-be-in-a-circular-orbit-at-this-height-is-e2-the-value-of-h-for-which-e1-and-e2-are-equal-is/