According to Newton, the gravitational acceleration of a spherical body is given by
$$a = \frac{GM}{r^2}$$
where $GM$ is the standard gravitational parameter and $r$ is the radial distance from the centre of the sphere. Jupiter has high rotation, so it's a bit squashed (it's an oblate spheroid), but the above formula is still a good approximation.
It's not easy to determine the internal structure of a giant planet, so the surface of a giant planet is usually defined to be where the the atmospheric pressure is $1$ bar (which is approximately the air pressure at Earth's surface). As I mentioned here, it appears that Jupiter has a diffuse core, but the details are still hazy.
From the JPL Horizons body data page for Jupiter, it has an equatorial radius of $71492\pm4 \,{\rm km}$. Its gravitational parameter is $126686531.900 \,{\rm km^3/s^2}$.
Using those numbers, the surface acceleration is approximately $24.7865 \,{\rm m/s^2}$, which is consistent with the value given by Horizons. Incidentally, the centrifugal acceleration at that radius is approximately $ 2.21 \,{\rm m/s^2}$.
To find the radius where $a$ equals the standard Earth gravitational acceleration, $g=9.80665 \,{\rm m/s^2}$, we can use
$$r = \sqrt{\frac{GM}{g}}$$
That gives $r\approx 113659 \,{\rm km}$, which is roughly $42167 \,{\rm km}$ above the nominal surface. The scale height of Jupiter's atmosphere is ~$27 {\rm km}$, so the atmospheric pressure at that altitude is negligible.
As JamesK mentions, the only way to maintain that altitude without using a rocket continuously burning a lot of fuel is to be in orbit, and of course an orbiting body is in freefall, so it doesn't feel the gravitational acceleration.
The speed of a body in a circular orbit at that altitude is ~$33.4 \,{\rm km/s}$, which is a little faster than Earth's orbital speed around the Sun (~$29 \,{\rm km/s}$). The period of that orbit is almost $6$ hours.
The escape velocity at that altitude is ~$47.2 \,{\rm km/s}$, which is much faster than the escape velocity at Earth's surface, ~$11.2 \,{\rm km/s}$.
Orbit speeds can be calculated from the gravitational potential, which is the gravitational potential energy per unit mass. It's given by
$$V = -\frac{GM}{r}$$
The circular orbit speed is
$$v_c = \sqrt{\frac{GM}{r}}$$
and escape velocity is
$$v_e = \sqrt{\frac{2GM}{r}}$$
The radius where Jupiter's gravitational potential equals the gravitational potential on Earth's surface is a little over $2$ million kilometres.