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This review examines non-equatorial space elevators, analyzing tether mechanics and implications for anchor locations.
Non-equatorial space elevators are interesting as they give more freedom for anchor location, avoid the highly occupied geosynchronous orbit and the areas of highest radiation in the Van Allen belts. We review the static equation for a uniform-stress tether, and use it to study the tapering of a uniform-stress tether in a general potential field. We then focus on a rotating coulomb potential and study the range of latitudes that are allowed for a uniform-stress space elevator. Finally, we look at a few practical issues that are raised by non-equatorial space elevators.
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Blaise Gassend (2025) studied this question.
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