00:01
Well, in an elliptic orbit, the total system energy is conserved and energy remains the same.
00:13
So, u is equal to k, which is kinetic energy plus gravitational potential energy plus internal energy is equal to k.
00:33
Well, k is a constant.
00:37
The velocity is not uniform, however, and the satellite slows down, losing kinetic energy at the far -best position from the earth on the trajectory.
00:49
And conversely, the satellite speeds up as it closes the radial distance to earth.
00:56
So any loss or gain in the system's kinetic energy is counterbalanced by the change in systems, gravitational potential energy so in general for an elliptic orbit initial kinetic energy is not equal to final kinetic energy and also initial gravitational potential energy is not equal to final gravitational potential energy but the total energy is always a constant so if we examine the equation for the gravitational potential of the system well, initial gravitational potential energy is given by minus capital g, or capital g is the gravitational constant, times mass of earth times mass of satellite divided by the radius...