Two-body Keplerian orbit propagation
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kepler: fix README — remove Vec3 section (belongs to separate package)

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README.md
··· 24 24 25 25 ## API Overview 26 26 27 - ### `Vec3` 28 - - **`type t`** -- 3D vector: `x`, `y`, `z` 29 - - **`add`**, **`sub`**, **`scale`**, **`dot`**, **`cross`**, **`length`** 30 - 31 27 ### `Analytic` 32 28 - **`precompute`** -- Convert state vector to orbital elements (call once) 33 29 - **`at_precomputed`** -- Propagate from precomputed elements (~20 FLOPs)