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Questions regarding the mechanics or attributes of objects falling 'around' other objects, thereby orbiting them.

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How to find ECI coordinates for a circular orbit

Suppose a satellite is orbiting Earth in a circular orbit, of which I know the inclination $i$, the right ascension of the ascending node $\Omega$, the semi-major axis $a$ (or orbit radius given that it … is a circular orbit), the angular velocity of spacecraft in the orbit $n$. …
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