Two satellites are in circular orbits around the earth. The orbit for satellite A is at a height of 360 km above the earth's surface, while that for satellite_B is at a height of 720 km. Find the orbital speed for each satellite. 360 x 10°m 720 x 10°m Known: - 360km = r6 =720kn TA =?? To= ? For urrulau s ĜhM GM = v² Unknown: Strategy: V= 2nえT But 4222 3

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Chapter1: Units, Trigonometry. And Vectors
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Modeled after the two satellites problem (slide 12 in Lecture13, Universal gravity), imagine now if the period of the satellite is exact 93.55 hours, the earth mass is 5.98 x 1024 kg, and the radius of the earth is 3958.8 miles, what is the distance of the satellite from the surface of the earth in MILES? Use G=6.67x 10 -11 Nm2/kg2. Your answer for this problem is some large number on the order of 105 to 106. Just put in the raw number as your answer. For example, 34567.11.

Two satellites are in circular orbits around the earth. The orbit for
satellite A is at a height of 360 km above the earth's surface, while
that for satellite_B is at a height of 720 km. Find the orbital speed
for each satellite.
360 X103m
720 x 10°m
Known:
- 360km =
r6 = 720kn
TA =?? Tg= ?
For urrulau s ĜhM
GM = v2
Unknown:
Strategy:
V= 2nえT
But
3
Transcribed Image Text:Two satellites are in circular orbits around the earth. The orbit for satellite A is at a height of 360 km above the earth's surface, while that for satellite_B is at a height of 720 km. Find the orbital speed for each satellite. 360 X103m 720 x 10°m Known: - 360km = r6 = 720kn TA =?? Tg= ? For urrulau s ĜhM GM = v2 Unknown: Strategy: V= 2nえT But 3
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