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Question #254000
What is the speed of a satellite moving in a circular orbit at a height of 3800km above the
surface of the earth? (b) what is the period of the satellite in hours? The mass of the
earth is 5.97x10^24 kg. The radius of the earth is 6.38x10^6 m
Expert's answer
(a) Determine the speed:
G
M
m
/
(
R
+
H
)
2
=
m
v
2
/
(
R
+
H
)
,
v
=
G
M
R
+
H
=
6255
m/s
.
GMm/(R+H)^2=mv^2/(R+H),\\\space\\ v=\sqrt\frac{GM}{R+H}=6255\text{ m/s}.
GM
m
/
(
R
+
H
)
2
=
m
v
2
/
(
R
+
H
)
,
v
=
R
+
H
GM
=
6255
m/s
.
(b) The period is
T
=
L
/
v
=
2
π
(
R
+
H
)
/
v
=
10226
s, or 2 h 50 min
.
T=L/v=2\pi (R+H)/v=10226\text{ s, or 2 h 50 min}.
T
=
L
/
v
=
2
π
(
R
+
H
)
/
v
=
10226
s, or 2 h 50 min
.
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