a satellite is in orbit about the Earth at a height of 2500 km above the surface of the Earth. If the radius of the Earth is 6370 km, what is the radius of the satellite’s orbit? Recall that r = RE + H. In #1, what is the period of the satellite’s orbit in hours? It may be helpful to remember that G = 6.67 × 10−11 kg−1m3s−2, while ME = 5.96 × 1024 kg. In addition recall that the formula for the orbital period is: ⃝ A. 2.31 hours ⃝ B. 3.59 hours ⃝ C. 5.12 hours ⃝ D. 8.27 hours

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#1 Orbital Dynamics
Suppose a satellite is in orbit about the Earth at a height of 2500 km above the surface of the Earth. If the radius of the Earth is 6370 km, what is the radius of the satellite’s orbit? Recall that r = RE + H.

In #1, what is the period of the satellite’s orbit in hours? It may be helpful to remember

that G = 6.67 × 10−11 kg−1m3s−2, while ME = 5.96 × 1024 kg. In addition recall that the

formula for the orbital period is:

⃝ A. 2.31 hours ⃝ B. 3.59 hours ⃝ C. 5.12 hours ⃝ D. 8.27 hours

? r3
T=2π GM (1)

 

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