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A satellite is to be placed in a circular orbit above the Earth’s surface
PHYSICS · Subjective · CBSE · Physics · Gravitation · Gravitation
Problem
A satellite is to be placed in a circular orbit
400
km
400\,\text{km}
400
km
above the Earth’s surface. Take Earth’s radius
R
E
=
6.4
×
10
6
m
R_E = 6.4\times10^{6}\,\text{m}
R
E
=
6.4
×
1
0
6
m
, Earth’s mass
M
E
=
6.0
×
10
24
kg
M_E = 6.0\times10^{24}\,\text{kg}
M
E
=
6.0
×
1
0
24
kg
and
G
=
6.67
×
10
−
11
N m
2
/kg
2
G = 6.67\times10^{-11}\,\text{N m}^2\!\text{/kg}^2
G
=
6.67
×
1
0
−
11
N m
2
/kg
2
. Calculate its orbital speed, giving your answer to one decimal place in
km s
−
1
\text{km s}^{-1}
km s
−
1
.
Related theory
Satellites & Orbital Motion
Gravitation
Orbital velocity and period
Earth satellites
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