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Physics
Problem
A satellite revolves around Mars in a circular orbit with speed
3.0
km/s
3.0\,\text{km/s}
3.0
km/s
. Given the Martian radius
R
M
=
3390
km
R_M = 3390\,\text{km}
R
M
=
3390
km
and
G
M
M
=
4.24
×
10
13
m
3
s
−
2
GM_M = 4.24 \times 10^{13}\,\text{m}^3\text{s}^{-2}
G
M
M
=
4.24
×
1
0
13
m
3
s
−
2
, determine its altitude above the Martian surface. a)
800
km
800\,\text{km}
800
km
b)
4.7
×
10
3
km
4.7\times10^{3}\,\text{km}
4.7
×
1
0
3
km
c)
1.3
×
10
3
km
1.3\times10^{3}\,\text{km}
1.3
×
1
0
3
km
d)
470
km
470\,\text{km}
470
km
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