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A linear model is developed to predict the reentry time for spacecraft in circular, low Earth orbits (LEO) using data from two line element (TLE) sets.

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This page is a summary of: Linear Model for Reentry Time Prediction of Spacecraft in Low-Eccentricity, Low Earth Orbits, Journal of Spacecraft and Rockets, March 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.a34334.
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