I think I see what they were getting at. The Apoapsis is the farthest part of the craft's orbit. It burns up at the opposite point, the nearest part of it orbit ,approximately half way through its total orbit. The time lapse between those times given is is 3 days, five hours, and 5 minutes or $277,500s$. Double that to get the full period: $555,000s$
$G=6.6743e^{-11}m^3/(kgs^2)$
Assuming a circular orbit:
$a=1.3\cdot 10^9m$
$\frac{4\pi^2a^3}{GT^2}\implies M_s=4.2188\cdot 10^{27} Kg$
Assuming as per Michael Seifert's suggestion $a=(1/2)1.3\cdot 10^9m $
then implies $M_s=5.27\cdot 10^{26}$
https://science.nasa.gov/mission/cassini/grand-finale/grand-finale-orbit-guide/ gives the orbital period for Cassini the last several weeks of its adventure is 6.5 days or $561500$ seconds.
5.683 × 10^26 kg is the mass of Saturn from Google.
$(5.683-42.188)/5.683*100\%=-642.354\%$ : per cent error for circular orbit.
$(5.683-5.27)/5.683*100\%=7.26\%$: per cent error of highly elliptical orbit.
Not as accurate as I'd like.
I could see sources of error, assuming I got the arithmetic right this time.
The period estimate I used comes from assuming a circular orbit so not a highly eccentric one. That alone might account for much of the error as mentioned by Michael Seifert in the comments. I'm also assuming a two body problem. Saturn has dozens of moons that might effect the period. Jupiter might be near enough and massive enough to change things up. Then how long was Cassini experiencing drag before contact was lost? Drag would throw off the period estimate.