equation 27.52 eq:cfs-orbit-integral
open in the book ·
parts/03-classical-mechanics/10-central-forces-statics.tex:1259
- part of a statement or proof
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step_from
equation 27.53
eq:cfs-kepler-third-exact
¶
- depends_on example 27.36 A satellite in low Earth orbit ¶
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| type | direction | node | provenance | where |
|---|---|---|---|---|
step_from |
← | eq:cfs-kepler-third-exact | declared — integrating the equal-area law over one revolution and eliminating $p$ and $L$ | parts/03-classical-mechanics/10-central-forces-statics.tex:1277 |