An artificial satellite is a man-made body placed
in orbit around the earth
or another planet to
collect information
about it or communicate.
The International Space
Station is an example of
an artificial satellite.
Artificial satellitesorbiting the Earth
are a familiar part
of modern
technology.
A circular orbit is the simplest case. Circular orbital motion is when an object moves in a circular path around the center of mass of a system.
The only force acting on a satellite in a circular orbit
around the earth is the
earth’s gravitational
attraction, which is
directed toward the
center of the earth and
hence toward the center
of the orbit.
This means that the satellite is in
uniform circular motion and its speed is constant.
The satellite isn’t falling toward the earth; rather,
it’s constantly falling
around the earth. In a
circular orbit, the speed
is just right to keep the
distance from the
satellite to the center of
the earth constant.
In a circular orbit, the following
quantities are
constant: distance,
speed, angular
speed, and
potential and
kinetic energy.
Earth’s actual: Mass = 5.972x10^24 kgs
radius = 6.38 x10^6 m
Gravitational force. Note: Fg = Fc (centripetal
force)
Fg = G Mm / r^2
where;
Fg = gravitational force
G = gravitational constant
M = mass of the Earth
m = mass of the satellite
Radial acceleration -acceleration of the
satellite
arad = mv^2 / r
where;
arad = radial acceleration
m = mass
v = velocity
r = radius
Formula = arad Note: (m) or mass in the a rad
equation will be diminished or
removed because the orbital
motion of the satellite does not
depend on its mass.
v= √Gm/r
This relationship shows that we can’t choose the orbit radius r and the speed
independently; for a given radius r, the
speed for a circular orbit is determined
The satellite’s mass (m) doesn’t appear in the equation above, which shows that
the motion of a satellite does not
depend on its mass. If we could cut a
satellite in half without changing its
speed, each half would continue on with
the original motion.