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For stable orbit @ 6 700 000 metres

Velocity = sq. root ( G * mass earth / orbit radius ) = 7713.576 metres / sec

Time for (sidereal) orbit = (2 * pi * radius) / velocity = 5457.56 seconds.

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12y ago
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Wiki User

13y ago

it is 88.5 minutes

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Anonymous

Lvl 1
4y ago

88.5 minutes

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Q: The moon revolves around the earth once every 27.3 days and is 390.000 km from the center of the earth how long would it take a satellite launched to a distance of 6.700 km from the center of the eart?
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