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// Chapter 11 example 10
//------------------------------------------------------------------------------
clc;
clear;
// Given data
e = 0.5; // orbit eccentricity
ae = 14000; // from fig. the distance from center of ellipse to the centre of earth
// Calculations
a = ae/e; // semi major axis
apogee = a*(1 + e); // Apogee in km
perige = a*(1 - e); // perigee in km
// output
mprintf('Apogee = %d km\n Perigee = %d km',apogee,perige);
//------------------------------------------------------------------------------
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