Here's the orbit in the TEME reference frame obtained from the TLE shown above propagated with the SGP4/SDP4 propagator; please, take a look
here for further details.
The reference direction (the mean equinox of date) is represented by the +X axis direction.
The label that appears when you hover the mouse over a point shows: UTC time, radius vector (km), inertial orbital speed (m/s), latitude and longitude (degrees), altitude above the WGS-72 ellipsoid (km).
Here's the same graph as above but in the ECEF reference frame.
The popup label shows: UTC time, radius vector (km), ECEF orbital speed (m/s), latitude and longitude (degrees), altitude above the WGS-72 ellipsoid (km).