A satellite is arbithng a planet of a fathes of 5500 km from the planet's centen If Its ofbital veloelty \( 18250 \mathrm{~m} / \mathrm{s} \) deternine the inme pethat of the sotellite's motlon in hours
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To determine the time period of the satellite's motion, we can use the formula for the orbital period \( T \): \[ T = \frac{2\pi r}{v} \] where \( r \) is the orbital radius and \( v \) is the orbital velocity. Given: - \( r = 5500 \, \text{km} = 5500000 \, \text{m} \) - \( v = 18250 \, \text{m/s} \) Now we plug in the values: \[ T = \frac{2\pi (5500000)}{18250} \] Calculating the numerator: \[ 2\pi (5500000) \approx 34557500.74 \, \text{m} \] Now, dividing by the velocity: \[ T \approx \frac{34557500.74}{18250} \] This gives us: \[ T \approx 1893.2 \, \text{s} \] Now, to convert seconds into hours: \[ T \approx \frac{1893.2}{3600} \approx 0.526 \, \text{hours} \] So, the orbital period of the satellite is approximately 0.526 hours.