A LEO satellite was launched into an orbit at an altitude of 1000 km. The satellite orbits the earth at a speed given by: GME km/s h+ RE Given the earth radius 6371 km and Kepler's constant 3.986 x 105 km³/52 Calculate the time taken by the satellite, in hours, to travel 7 orbital periods. Do not include the units in the answer box. Give your answer rounded to two decimal places.
A LEO satellite was launched into an orbit at an altitude of 1000 km. The satellite orbits the earth at a speed given by: GME km/s h+ RE Given the earth radius 6371 km and Kepler's constant 3.986 x 105 km³/52 Calculate the time taken by the satellite, in hours, to travel 7 orbital periods. Do not include the units in the answer box. Give your answer rounded to two decimal places.
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![A LEO satellite was launched into an orbit at an altitude of 1000 km. The satellite orbits the earth at a speed given by:
GME
km/s
h+ RE
Given the earth radius 6371 km and Kepler's constant 3.986 × 105 km³/2
Calculate the time taken by the satellite, in hours, to travel 7 orbital periods.
Do not include the units in the answer box. Give your answer rounded to two decimal places.](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2Ffe17cd79-4564-4c51-958f-a871ce15295b%2F192c4a8d-e28d-4864-a5df-ac61633b64a0%2F5616pbc_processed.png&w=3840&q=75)
Transcribed Image Text:A LEO satellite was launched into an orbit at an altitude of 1000 km. The satellite orbits the earth at a speed given by:
GME
km/s
h+ RE
Given the earth radius 6371 km and Kepler's constant 3.986 × 105 km³/2
Calculate the time taken by the satellite, in hours, to travel 7 orbital periods.
Do not include the units in the answer box. Give your answer rounded to two decimal places.
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