Just for grins, I found four historical element sets for the F9H/Tesla during its parking orbit:
1 43205U 18017A 18037.94171953 +.01086538 -52473-6 +58861-2 0 9998
2 43205 029.0166 287.3637 3402738 180.0678 179.9492 08.75207321000009
1 43205U 18017A 18037.94171962 .02159520 -54079-6 11669-1 0 9999
2 43205 29.0166 287.3643 3402882 180.0750 179.9361 8.75195074 03
1 43205U 18017A 18037.94189123 .00000283 -50857-6 00000+0 0 9991
2 43205 29.0185 287.3580 3404246 180.0270 180.5840 8.75540848 00
1 43205U 18017A 18037.94189123 .00000283 -50857-6 00000+0 0 9991
2 43205 29.0185 287.3580 3404246 180.0270 180.5840 8.75540848 00
Interpretation of the last set: 43205 is the NORAD catalog number.
2018-017A is the international designator (17th launch of 2018, primary object).
The time at which the elements are valid is year 2018, day 37 plus 0.94189123 days (UTC).
The orbital inclination is 29.0185 degrees, slightly more than the latitude of the launch site -- so the launch was nearly due east.
The right ascension of the ascending node (northbound equator crossing) is 287.3580 degrees. This is set by the sidereal time of the launch, which had been delayed a few hours.
The eccentricity is 0.3404246. Zero is circular, >=1 is escape (though NORAD doesn't do escaped objects).
The argument of perigee is 180.0270 degrees, so both perigee and apogee were over the equator. Typical for geostationary comsat launches.
The mean anomaly at epoch is 180.5840 degrees, so at the cited epoch time, the satellite was slightly past apogee.
The mean motion was 8.75540848 rev/day. Dividing it into 1440 minutes/day, that's 164.47 minutes, or two hours 44.47 minutes.
When I found it during the parking orbit the object wasn't named so I had to figure out which element set was likely to be the F9H/Tesla. The unusual period stood out, and the other numbers were pretty much as expected so I figured this had to be it.