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I understand the Repeat Ground Track (RGT) period of a satellite will be affected by its altitude. A similar post: How Do I determine the ground track period of a LEO satellite, describes a simple approach to determine the RGT period by using the ratio of the rotation periods of the planet and spacecraft. My question is whether other orbital parameters would as well, and how?

For instance, a satellite at 574km (and thus having an orbital period of 5,760s) could have a RGT period of 3 or 4 days [since the earth's rotation period of 86,400s times 3 and 4 are both multiples of 5,760]. If that's the case, surely altitude is not the only factor affecting the RGT period?

Shawn Lim
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Along with orbital dynamics there may be some commercial factors for anything advertised as re-visit rate rather than just repeat ground track rate.

Assuming this is a sun-synchronous orbit given the altitude the advertised re-visit rate may be limited by potentially other users consuming pointing time, storage or downlink availability, especially if this is a public facing/low cost service selling spare capacity of a constellation paid for by a primary/priority customer.

GremlinWranger
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