@spec fit_tle(
  [map()],
  keyword()
) :: {:ok, Sidereon.SGP4.Fit.t()} | {:error, term()}

Fit a TLE to TEME position samples using the core inverse-SGP4 solver.

@spec propagate(Sidereon.Elements.t(), DateTime.t()) ::
  {:ok, Sidereon.TemeState.t()} | {:error, propagation_error()}

Propagate a TLE to a specific datetime, returning a TEME state vector.

Uses the sgp4 Rust crate in AFSPC compatibility mode. Elements are passed as individual fields, so this works for both TLE and OMM inputs.

Returns {:ok, %Sidereon.TemeState{}} with position in km and velocity in km/s, or {:error, reason}.

@spec propagate_batch([Sidereon.Elements.t()], [number()], keyword()) ::
  {:ok, ok: [Sidereon.TemeState.t()], error: term()} | {:error, term()}

Propagate many satellites across a shared list of times, in one NIF call.

Each time is minutes since that satellite's own epoch (the core batch convention), so element i of the result is the arc for satellites |> Enum.at(i) evaluated at every offset in times_minutes. This is the throughput primitive over sidereon_core::astro::sgp4::propagate_batch; one bad satellite never collapses the batch.

satellites is a list of %Sidereon.Elements{}. Options:

• :opsmode - :afspc (default, matching propagate/2) or :improved.
• :parallel - when true, fans the per-satellite arcs across a thread pool (propagate_batch_parallel); the results are bit-identical to the serial path. Defaults to false.

Returns {:ok, arcs} where each arc is {:ok, [%Sidereon.TemeState{}, ...]} (one state per time, in order) or {:error, reason} for a satellite that failed to propagate. Returns {:error, {:invalid_elements, index, reason}} if an input element set cannot be marshalled.