Respuesta :
The formulas that will be used are:
Situation one:
The moon will be experiencing gravitational force in the form of centripetal force, so we equate the two formulas.
Gravitational force = GMm /r²
Centripetal force = mv²/r
Equating,
GMm/r² = mv²/r
v² = GM/r
The first scenario will use the formula v² = GM/r
Situation 2:
The second situation will use the simple distance over time formula for velocity, where the distance will be the circumference and the time will be in seconds.
v = 2rπ/t
Situation one:
The moon will be experiencing gravitational force in the form of centripetal force, so we equate the two formulas.
Gravitational force = GMm /r²
Centripetal force = mv²/r
Equating,
GMm/r² = mv²/r
v² = GM/r
The first scenario will use the formula v² = GM/r
Situation 2:
The second situation will use the simple distance over time formula for velocity, where the distance will be the circumference and the time will be in seconds.
v = 2rπ/t
The tangential speed of the satellite above the Earth's surface is [tex]7.588 \times 10^3 \ m/s[/tex].
Tangential speed
The tangential speed of an object around a circle is the linear speed of the object.
[tex]v = \omega r\\\\v = \frac{2\pi r }{T}[/tex]
The tangential speed of a satellite at the given radius and time is calculated as follows;
[tex]v = \frac{2\pi \times (150 \times 10^3 \ + \ 6371 \times 10^3)}{90 \times 60} \\\\v = 7.588 \times 10^3 \ m/s[/tex]
Thus, the tangential speed of the satellite above the Earth's surface is [tex]7.588 \times 10^3 \ m/s[/tex].
Learn more about tangential speed here: https://brainly.com/question/4387692