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How to calculate the time of a revolution or the speed of a satellite revolving around the earth in a stable orbit 1400 km from the earth?
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- ZardozLv 74 years agoFavorite Answer
P = √(4π²r³/GM)
vₒ = √(GM/r)
r is in meters from Earth's center.
r = 6.372[6] + 1.4[6] = 7.77[6] meters
GM = 3.986[14]
With the answer returned in m/s.
Source(s): [n] = 10ⁿ - Anonymous4 years ago
Hmm! More data is needed
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