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A Satellite in a 100-Mile-High Circular Orbit Around Earth Has 2\sqrt { 2 }

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A satellite in a 100-mile-high circular orbit around Earth has a velocity of approximately 17,500 miles per hour.If this velocity is multiplied by 2\sqrt { 2 } , the satellite will have the minimum velocity necessary to escape Earth's gravity and will follow a parabolic path with the center of Earth as the focus.(Hints: The radius of Earth is 4000 miles.)  A satellite in a 100-mile-high circular orbit around Earth has a velocity of approximately 17,500 miles per hour.If this velocity is multiplied by  \sqrt { 2 }  , the satellite will have the minimum velocity necessary to escape Earth's gravity and will follow a parabolic path with the center of Earth as the focus.(Hints: The radius of Earth is 4000 miles.)     Find the distance between the surface of the Earth and the satellite when  \theta = 50 ^ { \circ }  .  A) Distance between surface of Earth and satellite:4496 miles B) Distance between surface of Earth and satellite:4322 miles C) Distance between surface of Earth and satellite:1286 miles D) Distance between surface of Earth and satellite:643 miles E) Distance between surface of Earth and satellite:1492 miles Find the distance between the surface of the Earth and the satellite when θ=50\theta = 50 ^ { \circ } .


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