
#1
Jun2312, 10:54 AM

P: 344

When a satellite is affected by resistance against orbit motion,
for example from thin atmosphere or solar wind, it will as a result of this decelerates  but in that process it will decrease slightly toward the earth, and therefore following accelerate too. How can the new orbit speed be calculated? 



#2
Jun2312, 11:16 AM

PF Gold
P: 946

You may want to search and read up on the concept of "orbital decay" to get an idea of how orbital mechanics works in the presence of drag forces.




#3
Jun2312, 11:35 AM

P: 344

Let's say the resistance against motion is 1E10m/s^2 Due to the resistance the satellite will decrease towards the Earth, and hence the orbit speed will also increase, as well as it will decrease due to the resistance. 



#4
Jun2312, 02:08 PM

PF Gold
P: 946

How to calculate orbit speed
From an assumed constant deceleration due to drag you can find the change in speed due to this deceleration simply by multiplying with time. In a more detailed calculation you would instead (numerically) integrate the instantaneous deceleration over a period of time, along with other accelerations, in order to get a more accurate trajectory of the satellite.
But I'm not sure why you'd want to know this? In general, as long as the change in speed is low enough for the satellite still to be in orbit, then the most significant effect of the drag at any particular point in the orbit is to reduce the orbital height at the opposite side of the orbit. This means that low drag generally acts to first circularize the orbit and then, when the orbit is mostly circular, to lower the overall height. Thus, the change in orbital speed due to drag is closely connected to the change in orbital height, and it is usually the orbital height, rather than speed, that is in primary interest when you look at orbital decay. 


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