Orbis.TemeState (Orbis v0.7.0)

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Represents the position and velocity of a satellite in the TEME coordinate system.

TEME (True Equator Mean Equinox) is the reference frame used by SGP4 propagators.

Units

  • Position: kilometers (km) from Earth's center
  • Velocity: kilometers per second (km/s)

Summary

Types

t()

Types

t()

@type t() :: %Orbis.TemeState{
  position: {float(), float(), float()},
  velocity: {float(), float(), float()}
}