Obviously it isn't, though I'm not sure who you're really talking to in this thread with this comment. I do not think anyone claimed it was exceptional, like all the other fuels it's a trade off between various factors.
To give some considerations that can go in to choosing what to use as a fuel in a rocket.
Awhile ago I did read that methane was a bit harder to keep stable then some other fuels though and so a bit more of a detonation risk inside the engine. Though I guess with increasing expertise and better modelling capabilities that is less of a risk then it once was. Another issue is obviously that high efficiency fuels tend to give less good thrust to weight ratios on engines, thus why hydrogen engines historically were often paired and still at times are paired at launch with SRB, just so there is some more force lifting the rocket up in the first minute or two. Fortunately over the decades technology has apparently advanced enough to make engines light enough and performant enough to make quite powerful methane engines, a factor that might also be contributing in current interest in it. Especially as I believe for now hydrogen engines still seem to be more limited there. Still historically speaking this would have thus made methane engines less interesting.
Some other factors beyond those two would be that methane can be made a liquid in a temperature range pretty close to liquid oxygen, which means you probably don't need different equipment for it. The similar temperature range means you don't need to make two fully separate tanks either, but can just make one larger tank with a barrier in it, this allows for a small weight saving, which is nice for a rocket. It's a bit more efficient then kerosene as well of course, though still well short of hydrogen. And as I mentioned before, one can easily enough make it synthetically in the future, so it should have a better long term future as a fuel then a fossil fuel derived one.
As a last potential longer term consideration, there is one more efficient and potent fuel cycle that one could use to burn things. Which would be to detonate the fuels, this has for a very long time been a big problem to do effectively though, but recently some advancement have seemed to make rotating detonation engines practical options. How ever I've heard those only so far work with hydrogen and methane, so they're some what limited fuel wise. Still they are supposed to give a reasonable boost in rocket ISP, though I've not really heard a solid figure on how much, but based on various things I did run in to I'd guess it would probably be somewhere in the 5-15 percent range. A boost that large would be quite substantial, though for now I only know of NASA having created a functional demonstrator. Still as such this might in decade be used to squeeze out a final improvement in chemical rocket engines efficiencies then.
In any case, I hope this helps clarify for you that rocket fuels are thought about in some more depth here then just basic pop-sci levels of knowledge.