State Vector Determination By A Single Tracking Satellite

Kerry M. Soileau

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arXiv · 0705.1155

State Vector Determination By A Single Tracking Satellite

Kerry M. Soileau

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Abstract

Using only a single tracking satellite capable of only range measurements to an orbiting object in an unknown Keplerian orbit, it is theoretically possible to calculate the orbit and a current state vector. In this paper we derive an algorithm that can perform this calculation.

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Kerry M. Soileau. 2022-08-26. State Vector Determination By A Single Tracking Satellite. https://arxiv.org/abs/0705.1155

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