Respuesta :
The period of a satellite in a circular orbit can be obtained by using the formula below:
P = √(4π²r³/GM)
Where: constant GM of the Moon (gravity * mass) = 4.903x10^12 m³/s²
Substituting and simplifying:
P = 2.838x10^(-6) * √(1.738x10^6)³
P = 6502 seconds, or 108.37 minutes
P = √(4π²r³/GM)
Where: constant GM of the Moon (gravity * mass) = 4.903x10^12 m³/s²
Substituting and simplifying:
P = 2.838x10^(-6) * √(1.738x10^6)³
P = 6502 seconds, or 108.37 minutes