Open-space-toolkit-astrodynamics

**refactor**
- change the index returned by pass map to be the last index (323)

**feat**
- add repropagation of intermediate states to sequence and segment (316)
- add orbit pass computation logic (318)

**fix**
- set instant from inputs in NumericalSolver::integrateTime (320)

**feat**
- add argument of latitude options to Orbit::SunSynchronous (319)

**feat**
- Tabulated dynamics for custom contribution profiles (317)

* feat: add `AttitudeQuaternion` and `AngularVelocity` coordinate subsets and `State` constructors
* feat: enrich and fix time conversion functions
* fix: time conversion functions
* fix: update Propulsion System scalar constructor
* fix: py unit test packaging and enhance dev container formatting
* fix: non-root dev container ostk data issue
* fix: doxygen formatting
* docs: satellite system python docs
* docs: align sequence api docs with function definition


**Full Changelog**: https://github.com/open-space-collective/open-space-toolkit-astrodynamics/compare/5.1.5...5.2.0