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A
satellite in elliptical orbit follows an oval-shaped path. One part of
the orbit is closest to the centre of Earth (perigee) and the other part
is farthest away (apogee). A satellite in this orbit takes about 12
hours to circle the planet.
An ellipse can be long and skinny. An
ellipse can be very round. Scientists need a way to describe how round
or "stretched out" an ellipse is. They use a number to describe this,
and call it the "eccentricity" of the ellipse. Eccentricity is always
between zero and one for an ellipse. If it is close to zero, the ellipse
is nearly a circle. If it is close to one, the ellipse is long and
skinny.
An elliptical orbit can be useful to a
communications satellite because it allows the satellite to travel over
a specific region for a long portion of its orbit, and it is only out of
contact with that region for a short time when it is zipping quickly
around the other side of the Earth.
In 1600 Kepler became assistant to Tycho
Brahe who was making accurate observations of the planets. After Brahe
died in 1601 Kepler continued the work, calculating planetary orbits to
unprecedented accuracy.
Kepler showed that a planet moves round the Sun in an elliptical orbit
which has the Sun in one of its two foci. He also showed that a line
joining the planet to the Sun sweeps out equal areas in equal times as
the planet describes its orbit. Both these laws were first formulated
for the planet Mars, and published in Astronomia Nova (1609). |