# `Sidereon.OrbitDetermination.OrbitFitSolution`
[🔗](https://github.com/neilberkman/sidereon-ex/blob/main/lib/sidereon/orbit_determination.ex#L29)

Initial-state orbit fit for one satellite.

# `t`

```elixir
@type t() :: %Sidereon.OrbitDetermination.OrbitFitSolution{
  covariance: Sidereon.OrbitDetermination.OrbitFitCovariance.t(),
  fit_rms_3d_m: float(),
  geometry_quality: map(),
  initial_state: map(),
  iterations: non_neg_integer(),
  satellite: String.t(),
  seed_rms_3d_m: float()
}
```

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*Consult [api-reference.md](api-reference.md) for complete listing*