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this is if it is not a geostationary orbit, in which case it is always in the same place relative to earth.

imagine a circle of radius 42250km+radius of earth(6,356km). it's perimeter is

2 x pi x 48606km = satellite's journey.

then think of a really fast speed, which is the speed the satellite is moving at.

divide the distance by speed and you have the time of one orbit

However, by the height being 42250

, it makes me think the satellite is a geostationary satellite and so it would take 24 hours moving at approximately 12725 kmph

does that answer your question?

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