Question: Show through computations, that the eclipse period of a typical Space Shuttle orbit (200 km altitude circular orbit inclined at 28) when the orbit

Show through computations, that the eclipse period of a typical Space Shuttle

Show through computations, that the eclipse period of a typical Space Shuttle orbit (200 km altitude circular orbit inclined at 28) when the orbit plane contains the Earth-Sun vector is -36.9 min for a 10 step in 8.

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