- #1
Bjarne
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When a satellite is affected by resistance against orbit motion,
for example from thin atmosphere or solar wind, it will as a result of this decelerates -
but in that process it will decrease slightly toward the earth, and therefore following accelerate too.
How can the new orbit speed be calculated?
for example from thin atmosphere or solar wind, it will as a result of this decelerates -
but in that process it will decrease slightly toward the earth, and therefore following accelerate too.
How can the new orbit speed be calculated?
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