ok so because you dont seem to be understanding the astronomical difference in velocity between a plane, a missile, and a satellite ill go through the comparison. in the most favorable possible terms. choosing the AIM-54 phoenix missile because its the fastest missile i was able to find with a quick search.

F15 maximum speed: 738 m/s

AIM-54 Phoenix maximum speed: 1700 m/s

Low earth orbit velocity: 8700 m/s

so adding the plane and the missile together we get 2438 m/s, which means the missile would need to gain 6262 m/s of additional velocity to reach orbital velocity. this corresponds to an 11.7 times increase in kinetic energy.

so the F15 flies up, works as hard as it possibly can to get to maximum speed, then shoots its AIM-54 phoenix missile which uses all of its fuel to get to its maximum possible speed, a tiny nudge for maneuvering is going to add 11.7 times more kinetic energy and nearly quadruple its speed… yeah that missile could hit a satellite, but it will never become a satellite itself.

all of this completely ignores the delta-v losses to gravity, steering, and drag required for an orbital insertion trajectory, so things get much much worse from here. if you’re actually interested in this i suggest you look up some youtube videos on orbital launch vehicles. or just believe whatever you want. the tyranny of the rocket equation is such that it doesnt really care what you think.