Expand description
SP3-anchored numerical orbit determination and residual ledgers.
The fit estimates one inertial Cartesian initial state per satellite from a batch of precise ephemeris samples. Input positions follow the SP3 convention: ITRS/ECEF meters at scale-tagged epochs. They are transformed to GCRS kilometers with the shared frame pipeline before the numerical propagator is evaluated. Reported residuals are projected into the propagated state’s RTN frame and accumulated per satellite and per constellation.
Structs§
- Orbit
ArcSpan - Arc span covered by a residual ledger.
- Orbit
FitOptions - Options controlling a precise-orbit fit.
- Orbit
FitReport - Batch orbit-fit report for one or more satellites.
- Orbit
FitSolution - Initial-state fit result for one satellite.
- Orbit
Residual Ledger - Residual RMS ledger, grouped by satellite and constellation.
- Orbit
Residual Stats - RTN residual RMS summary.
- Oriented
Precise Ephemeris State Sample - One ECEF SP3 state sample paired with the Earth orientation for that epoch.
Enums§
- Orbit
FitCovariance - State-covariance result for a fitted initial state.
- Orbit
FitError - Error returned by precise-orbit fitting.
Functions§
- fit_
all_ sp3_ precise_ orbits - Fit every satellite declared in a parsed SP3 product.
- fit_
precise_ ephemeris_ sample_ orbit - Fit one satellite from precise ephemeris samples.
- fit_
precise_ ephemeris_ sample_ orbit_ with_ initial_ state - Fit one satellite from precise ephemeris samples with a caller-supplied arc-start initial-state seed.
- fit_
precise_ ephemeris_ sample_ orbits - Fit selected satellites from precise ephemeris samples.
- fit_
precise_ ephemeris_ state_ sample_ orbit - Fit one satellite from ECEF state samples paired with Earth orientation.
- fit_
precise_ ephemeris_ state_ sample_ orbits - Fit selected satellites from ECEF state samples paired with Earth orientation.
- fit_
sp3_ precise_ orbit - Fit one satellite from a parsed SP3 product.
- fit_
sp3_ precise_ orbit_ with_ initial_ state - Fit one satellite from a parsed SP3 product with a caller-supplied arc-start initial-state seed.
- fit_
sp3_ precise_ orbits - Fit selected satellites from a parsed SP3 product.