itrf2icrf

pride.coordinates.itrf2icrf(eops: numpy.ndarray, epoch: astropy.time.Time) → numpy.ndarray

Rotation matrix from ITRF to ICRF

Parameters:

• eop – Earth Orientation Parameters

• epoch – UTC epochs at which to compute matrix

Returns:

Rotation matrix from ITRF to ICRF as (N, 3, 3) array