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The orbit of a certain a satellite has a semimajor axis of 4.0 x 107 m and an eccentricity of 0.15. Its perigee (minimum distance) and apogee (maximum distance) are respectively
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The orbit of a certain a satellite has a semimajor axis of 4.0 x 107 m and an eccentricity of 0.15. Its perigee (minimum distance) and apogee (maximum distance) are respectively

User Raja Nagendra Kumar
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1 Answer

5 votes

Answer:

100KM and 1kkm

Step-by-step explanation:

User Prakhar Mittal
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