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Steffen Merseburg


Universität Stuttgart

Last seen: mer än 2 år ago Active since 2022

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How does the satellite scenario account for drag, if no drag coeffincient is passed?
Hello, I would like to simulate a couple of orbits from Keplarian Elements for a CubeSat. It all works fine except for i do not...

mer än 2 år ago | 1 answer | 0

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