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use cratebind;
/// Returns `angle` wrapped into the interval `[0, 2π)`.
///
/// # Arguments
///
/// * `angle` - The angle to wrap.
///
/// # Returns
///
/// The wrapped angle.
/// Converts mean anomaly to eccentric anomaly.
///
/// # Arguments
///
/// * `eccentricity` - The eccentricity of the orbit.
/// * `mean_anomaly` - The mean anomaly to convert.
///
/// # Returns
///
/// The eccentric anomaly.
/// Converts mean anomaly to true anomaly.
///
/// # Arguments
///
/// * `eccentricity` - The eccentricity of the orbit.
/// * `mean_anomaly` - The mean anomaly to convert.
///
/// # Returns
///
/// The true anomaly.
/// Converts eccentric anomaly to true anomaly.
///
/// # Arguments
///
/// * `eccentricity` - The eccentricity of the orbit.
/// * `eccentric_anomaly` - The eccentric anomaly to convert.
///
/// # Returns
///
/// The true anomaly.