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Calculate the linear velocity of an artificial Earth satellite at an altitude of 1700 km if its orbit can be considered approximately circular. Take the radius of the Earth 6400 km, acceleration of free fall 10 m/s^2.
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- Content type File
- Content description 25,56 kB
- Added to the site 05.06.2022
Additional description
A detailed solution with a brief note of the conditions, formulas and laws used in the solution, the derivation of the calculation formula and the answer.
If you have any questions about the solution, write. I try to help.
If you have any questions about the solution, write. I try to help.
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