Answers: 2
(1)
- Period of rotation of the satellite, measured in seconds. 
- Distance of the satellite with respect to the center of the planet, measured in meters. 
- Gravitational constant, measured in newton-square meters per square kilogram.
- Mass of the Earth, measured in kilograms.
![r = \sqrt[3]{\frac{G\cdot M\cdot T^{2}}{4\pi^{2}} }](/tpl/images/0891/6430/e5e24.png)
(2)
, 
and 
, then the distance of the satellite is:![r = \sqrt[3]{\frac{\left(6.67\times 10^{-11}\,\frac{N\cdot m^{2}}{kg^{2}} \right)\cdot (6.0\times 10^{24}\,kg)\cdot (25800\,s)^{2}}{4\pi^{2}} }](/tpl/images/0891/6430/9d36a.png)
(3)
- Mass of the satellite, measured in kilograms.
- Force exerted on the satellite by the Earth, measured in newtons.
and 
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A man-made satellite of mass 6105 kg is in orbit around the earth, making one revolution in 430 minu...
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