How does an object orbit something

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    Orbit
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Objects orbit due to the gravitational force acting at right angles to their direction of travel, creating a curved path instead of a straight line. When a satellite is launched, it must achieve a specific tangential velocity while ensuring its radial velocity approaches zero to enter orbit. The launch angle can influence this process, but rockets can also maneuver and adjust their velocity during ascent. Achieving a stable orbit typically requires multiple propulsion impulses or a sustained low-thrust burn. Understanding these principles clarifies why objects remain in orbit rather than moving in a straight line.
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I am having a very hard time understanding this concept in physics. Why would something orbit an object? Why doesn't it leave the orbit and move straight?

Also when a satellite leaves Earth how does it go into orbit? Does it have to be launched at a specific angle.
 
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Things can orbit because they experience a force that it at right angles to the direction they are traveling in.

You can see this on paper - mark a fat dot for the center of mass and a small dot for the satellite. Give the satellite a small random direction to travel. Now for each time interval, the satellite moves a small distance in the last direction it was headed in, but it is also attracted a small distance towards the fat dot. Try drawing that.

When a spacecraft goes into orbit, it's radial velocity has to reach zero and it's tangential velocity has to be right for the orbit. There are lots of ways of doing this - one way, indeed, involves being careful about the angle the rocket is launched. But recall, rockets are under power - they can, in principle anyway, manouver, and they can accelerate and decelerate. This gives more options.
 
ASidd said:
Why would something orbit an object? Why doesn't it leave the orbit and move straight?
Wiki article:

http://en.wikipedia.org/wiki/Orbit

ASidd said:
Also when a satellite leaves Earth how does it go into orbit? Does it have to be launched at a specific angle.
To get a satellite into a circular orbit normally requires at least two impulses, or one very long continuous (relatively low thrust) impulse. Wiki article:

Hohmann_transfer_orbit.htm
 
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