Hey Guys,
The things I understand:
1. GPS satellites orbit on six separate planes, all inclined at 55 degrees relative to the equator.
2. The Planes are inclined(?) relative to each other at increments of 60 degrees.
3. The GPS satellites orbit in a circular semi-sidereal 12-hour orbital period.
The things I don't understand:
1. How can an orbital plane be inclined relative to another orbital plane without changing its inclination relative to the equator?
2. How do you set these orbital parameters at launch?
3. If you don't get the launch perfect, where do you burn and in what orientation to rotate the orbital plane?
I made this diagram to help me understand it a little better, but aside from being able to make this in a 3D program, I still am having problems visualizing how to accomplish this goal.
Thanks guys, please let me know if I've forgot to include important pieces of the puzzle that I don't quite understand yet.
-Gary
The things I understand:
1. GPS satellites orbit on six separate planes, all inclined at 55 degrees relative to the equator.
2. The Planes are inclined(?) relative to each other at increments of 60 degrees.
3. The GPS satellites orbit in a circular semi-sidereal 12-hour orbital period.
The things I don't understand:
1. How can an orbital plane be inclined relative to another orbital plane without changing its inclination relative to the equator?
2. How do you set these orbital parameters at launch?
3. If you don't get the launch perfect, where do you burn and in what orientation to rotate the orbital plane?
I made this diagram to help me understand it a little better, but aside from being able to make this in a 3D program, I still am having problems visualizing how to accomplish this goal.
Thanks guys, please let me know if I've forgot to include important pieces of the puzzle that I don't quite understand yet.
-Gary
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