Questions on the movie Gravity (2013) To start off, I'm not a physicist but a programmer, and only had a few years of physics education in high school so I'm sorry if I'm asking a stupid question.
I just finished watching the movie Gravity (2013) and I found online already a whole list of things wrong with the movie, but there are two things that I think is wrong that I couldn't find:


*

*The premise of the movie is that a satellite is hit by a missle which causes debris setting off a chain reaction leading to the catastrophic destruction of space stations and space shuttles. Is it true that debris can stay in orbit at the same height as space stations, while having a very large relative speed to the space stations? It was my understanding that if the velocity of objects change, then also its orbit altitude (given a circular orbit), right?

*In the end, the main character gets to the Chinese space station, which is already deorbiting although it seems structurally intact. Is it possible for the intact station to deorbit, simply by getting a little bit hit (it couldn't have been much since it was still mostly intact)?

 A: *

*The satellite did not start in the ISS orbit, and not all orbits are circles.


The ISS orbit is free of large satellites.  So the fictional one from the movie was in a different orbit.  Therefore it's not too difficult to believe that debris from it would have a high relative velocity.  The debris might have been in a very elliptical orbit with a large range of altitudes.
It's not even necessary for them to have different altitudes.  As long as they intersect at an angle, the relative speeds will be very high.  (Much higher than would be useful for a movie).
That doesn't mean that the action depicted in the movie was accurate, just that any intersection would likely be at very high closing speeds.


*

*By large objects, no.


If the other space station had been hit by debris, it would have been damaged.  High-speed impacts can't change the momentum of the entire station much.  The material gives way before forces build up much, and the interaction time is low. 
Deorbit happens over a much longer period of time due primarily to atmospheric drag.  
A: 
Is it true that debris can stay in orbit at the same height as space stations, while having a very large relative speed to the space stations?

Most LEO objects orbit in the same direction, namely the direction the Earth rotates.  This is done to take advantage of the initial speed supplied by the Earth's rotation.  So the main velocity difference would likely be due to different inclinations (i.e., not in the same plane) or elliptical vs. circular orbits.
Let's make it simple and assume that two objects, E and I, both have circular orbits at the same altitude, thus they have the same orbital speed.  However, let us assume object I has an inclined orbit at some angle $\alpha$ to the equatorial plane and that they orbit in the same azimuthal direction.
Now the when we move into the frame of, say, the equatorial orbiting object the inclined object will appear to be coming from ahead of you.  If the inclined orbit is from south-to-north(north-to-south), then object I would appear to be coming at you from the south(north) and from ahead of you.  This is just from the vector subtraction, where:
$$
\mathbf{V}_{I} - \mathbf{V}_{E} = -\mathbf{V}_{rel} \tag{1}
$$
or
$$
\mathbf{V}_{E} = \mathbf{V}_{I} + \mathbf{V}_{rel} \tag{2}
$$
where $\lvert \mathbf{V}_{E} \rvert = \lvert \mathbf{V}_{I} \rvert$ we have defined:
$$
\begin{align}
\mathbf{V}_{E} & \sim V_{E} \ \hat{\mathbf{x}} \tag{3a} \\
\mathbf{V}_{I} & \sim V_{I} \left( \cos{\alpha} \ \hat{\mathbf{x}} + \sin{\alpha} \ \hat{\mathbf{y}} \right) \tag{3b}
\end{align}
$$
Note:  I really should be doing this in spherical trigonometry, but let's only concern ourselves with the immediate region of interaction so we can take the limit as the radius of curvature goes to infinity.
As you can see, $\mathbf{V}_{rel}$ is given by:
$$
\mathbf{V}_{rel} = V_{E} \left[ \left( 1 - \cos{\alpha} \right) \hat{\mathbf{x}} - \sin{\alpha} \hat{\mathbf{y}} \right] \tag{4}
$$
which shows that $\lim_{\alpha \rightarrow 0} \mathbf{V}_{rel} = 0$, as expected.
The maximum of $\lvert \mathbf{V}_{rel} \rvert$ occurs in the limit as $\alpha \rightarrow \pi/2$, which is $\sim \sqrt{2} \ V_{E}$.
The typical orbital speed of a LEO object is ~7-8 km/s (or ~25,200-28,800 kph = ~15,700-17,900 mph), so the maximum impact speed is going to be ~10-11 km/s (or ~35,600-40,700 kph = ~22,100-25,300 mph).
So the short answer to your question is yes.
If the objects were orbiting in opposite directions, then the maximum of $\lvert \mathbf{V}_{rel} \rvert$ would increase, of course.  Regardless, unless $\alpha \ll 1$, $\lvert \mathbf{V}_{rel} \rvert$ is going to be large for all intents and purposes.

Is it possible for the intact station to deorbit, simply by getting a little bit hit (it couldn't have been much since it was still mostly intact)?

I am going to guess no because of my response to the previous part.  A space station has a great deal of linear and angular momentum.  To exert enough force and torque to change those would require high impact speeds.  Since most of the space station's outer hull is very thin, the end result would not be the entire object being "shoved" to a different altitude.  Rather, the impacting object would probably just tear through the station and/or ablate on impact.
More Important Note
In the movie, the characters are able to see the objects moving towards them.  If we assume that the objects are moving at, say, $\alpha \sim \pi/6$ to the space station's plane, then $\lvert \mathbf{V}_{rel} \rvert \sim \sqrt{2 - \sqrt{3}} V_{E}$.  If we assume the same values as above for LEO orbits, then $\lvert \mathbf{V}_{rel} \rvert$ ~3.6-4.1 km/s (or ~13,000-14,900 kph = ~8,100-9,200 mph).
These values correspond to Mach ~ 10-12 at sea level.  For comparison, the muzzle velocity of a bullet from a high powered rifle varies from Mach ~ 1.8-3.6, depending on the caliber and model.
I am inclined to think that were this situation to really occur, a human would not be able to see the incident objects unless they were very large because of the lighting conditions and the speed at which the objects were moving.
A more accurate portrayal would have shown parts of the space station just disappearing and/or exploding.  There would not have been the nice, slow moving objects flying by that destroyed everything.
Update
When we look at the full range of muzzle velocities from a list of cartridges, we find handguns/pistols range from ~304–515 m/s and rifles range from ~600–1392 m/s.  I plotted the relative speed between two orbiting objects as a function of inclination (i.e., Equation 4 above) shown in the following image.

As shown, after even only ~3-4 degrees the speed differences exceed most handgun round muzzle speeds and after ~11 degrees nearly all civilian rifle rounds.
A: I'm not an expert either, but here are my thoughts.


*

*While object at orbit at the same height will have more or less the same speed, their direction are independent. Remember, the earth is a (3D) sphere, and you are not required to orbit over the equator. If two objects collide going in opposite directions the speed at the impact will be doubled!

*Objects at low orbits will decay, mainly because of the drag with the atmosphere traces. Take a look at the Orbital Decay article in Wikipedia. The ISS (or the CSS) have an orbit so low that if not pushed up periodically they will deorbit in just a couple of years. So my take is that the CSS is not deorbiting because of a hit, but just because it had been abandoned, just like the old Mir was.
