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| | Energy |
 | | Under standard assumptions, specific orbital energy () of elliptic orbit is negative and the orbital energy conservation equation for this orbit takes form: where: is orbital velocity of orbiting body, is radial distance of orbiting body from central body, is length of semi-major axis, is standard gravitational parameter. |
 | | Under standard assumptions, specific orbital energy () is negative and the orbital energy conservation equation for this orbit takes the form: where: is orbital velocity of orbiting body, is radius of orbit equal to radial distance of orbiting body from central body, is standard gravitational parameter. |
 | | Under standard assumptions, specific orbital energy () of a hyperbolic trajectory is greater than zero and the orbital energy conservation equation for this kind of trajectory takes form: where: is orbital velocity of orbiting body, is radial distance of orbiting body from central body, is length of semi-major axis,... |
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