Fermi
·
Concept Library
·
Courses
·
Books
·
Problems
·
Simulations
·
Math Wiki
·
High School
Fermi
›
Problems
Calculate the approximate orbital speed of a satellite placed above the Earth’s surface
PHYSICS · Single correct · CBSE · Physics · Gravitation · Gravitation
Problem
Calculate the approximate orbital speed of a satellite placed
400
km
400\,\text{km}
400
km
above the Earth’s surface. Take Earth’s radius
R
E
=
6.4
×
10
3
km
R_E = 6.4 \times 10^3\,\text{km}
R
E
=
6.4
×
1
0
3
km
and
G
M
E
=
3.99
×
10
14
m
3
s
−
2
GM_E = 3.99 \times 10^{14}\,\text{m}^3\text{s}^{-2}
G
M
E
=
3.99
×
1
0
14
m
3
s
−
2
. (a)
11.2
km/s
11.2\,\text{km/s}
11.2
km/s
(b)
6.2
km/s
6.2\,\text{km/s}
6.2
km/s
(c)
7.7
km/s
7.7\,\text{km/s}
7.7
km/s
(d)
8.2
km/s
8.2\,\text{km/s}
8.2
km/s
Related theory
Satellites & Orbital Motion
Gravitation
Orbital velocity and period
Earth satellites
Browse the problem library