Consider this equation for gravitational attraction between two bodies:
$$F = G \frac{m_1 m_2}{r^2}$$
where:
- $F$ is the force between the masses;
- $G$ is the gravitational constant (6.674×10−11 N · (m/kg)2);
- $m1$ is the first mass;
- $m2$ is the second mass;
- $r$ is the distance between the centers of the masses.
So if we say that an astronaut in an EVA suit has a mass of 150 kg, the International Space Station (ISS) itself has a mass of 390,000 kg, and the distance between their centers of mass is 5 meters, then their gravitational attraction between them is $1.042 × 10^{-6} \text{ m/s}^2$, or roughly one ten millionth (1/10,000,000) that of standard gravity at the surface of the Earth ($9.80665 \text{ m/s}^2$).
Now, neither the astronaut nor the station are point masses, so at such close proximity to each other, their mass distribution will play a major role and we have to account for it. Problem is, we don't really have exact mass distribution of the station, even if we neglected astronauts own non-uniformity as largely irrelevant due to small relative mass to the station. But, since we also don't have astronaut's angle to it, I'll just assume uniform mass for the 100 m long and 5 m in girth (r=2.5 m) station, and astronaut's position tangential to the station and orthogonal to its center of mass. I.e. the astronaut will be outside the station, somewhere near Node 1's outer truss;
In our case (with a few assumptions making this easier to calculate), combined gravity vector amplitude will change with cosine to the mean angle to the station's mass. That is, angle to the centroid of each 50 m sides. In our case, using the SOHCAHTOA mnemonic, that would be, 78.69°. So our acceleration to our uniform mass center of given dimensions and distribution would be $\text{cos}(78.69°) \cdot 1.042 × 10^{-6} \text{ m/s}^2$ or $2.04264874 × 10^{-7} \text{ m/s}^2$.
That is only $2.36349805 × 10^{-8}$ times (24 one billionths) the Earth's gravity at ISS mean orbital altitude (semi-major axis) of $\approx 8.64 \text{ m/s}^2$.
So not exactly nothing, but you'll grow a really long beard waiting for any noticeable change in your position relative to the station to happen due to your mutual gravitational attraction alone. Slight difference in your orbit relative to the station, combined with gravity gradient with respect to the station's center of mass will move you relative to it much faster than that, and we still call it a microgravity environment (i.e. difference measurable on a micro-g scale for its entire volume).
Also, for what is worth, distant gravitational perturbers like other celestial bodies will act on the station in exactly the same way as on our EVA astronaut, so their position relative to each other doesn't change because of that. There might be other, non-gravitational perturbing effects like solar wind, radiation pressure and exospheric drag, affecting station's movement slightly differently than our astronaut's, but that's not what the question asks.
Gravity is essentially a really weak force and it takes a whole lot of mass for its effects to be appreciable without doing extremely precise measurements (and growing a long beard). If you don't believe me, consider this: You can pick up relatively heavy objects off the Earth's surface while the whole planet is gravitationally pulling onto them. Conversely, take two small rare earth magnets, join them together by opposite magnetic poles, and you'll have really big problems separating them again.