Hi David_Queliz, and Welcome to the community!
You originally wrote:
And your most recent upload was:
As you implied 290kts is way lower than 457kts shown above.
IAS (indicated airspeed) is the 290kts. That is the “pressure speed”. It’s the speed your wings, flaps and fuselage “feel” from the air being thinner as you go higher (air molecules can be going past you much faster, but there are less of them, so the speed feels lower: there’s less impact force on the aircraft so it behaves like it’s actually travelling at that lower speed).
IAS is on your vertical speed strip on the left of the screen.
Your actual speed through the air gets much higher than IAS as you move increasingly into thinner air, and that’s what the 457kts comes from.
TAS (true airspeed) is your actual speed through the air. So, this is almost always a higher speed (often much higher), and is not affected by a steady wind speed (even if the wind could be 1000mph, TAS would be unaffected).
TAS is how fast the air molecules are actually moving past your aircraft (or how fast you are moving past the air molecules).
GS (ground speed) is TAS after adjusting for wind speed. So, both GS and TAS will often be much higher than IAS simply because you are flying high up in thin air (a 150 kts tail wind makes your ground speed that much higher).
From your other screen print:
You can actually see GS side by side with IAS, being much higher at 589kts compared to 333kts.
That big difference is almost all due to the thin air effect up at 26,900ft.
Notice we can’t tell directly from this how much the wind speed is making GS different from TAS.
Elsewhere, of course, you can check the windspeed that your own aircraft encounters (4kt tail wind here with GS 0 on the ground, of course):
(btw: mach speed as in 0.87 in your image, is TAS as a decimal fraction of the speed of sound. So that aircraft was travelling at 87% of the speed of sound in terms of how fast the air molecules are actually moving past your aircraft, even though the pressure speed, or IAS, is much lower than the speed of sound.
Since mach is a measure of TAS, it also does not change with wind speed.)