Can You Achieve a Circular Orbit with Non-Perpendicular Launch Velocities?

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To achieve a circular orbit around a planet, the launch velocity must be perpendicular to the radius vector at a distance R, specifically at Sqrt[Gm/R]. Launching at an angle introduces a non-perpendicular component, which affects the trajectory. The resulting orbit is likely to be elliptical rather than circular, as the perpendicular component remains the same but the angle alters the overall path. Therefore, a non-perpendicular launch velocity does not allow for a circular orbit. The conclusion is that any angled launch will result in an elliptical orbit.
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If you are at the distance R from a planet and you want to achieve a circular orbit your velocity must be Sqrt[Gm/R] perpendicular to the radius vector.

But what if you launch at an angle (ie no longer perpendicular to the radius)? Is it still possible to achieve a circular orbit if the perpendicular component is still Sqrt[Gm/R]?
 
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Mt guess is that you will end up with some sort of ellipse.
 
You will definitely have a non-circular ellipse.
 
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