A landing craft with mass $12,500 \mathrm{~kg}$ is in a circular orbit $5.75 \times 10^{5} \mathrm{~m}$ above the surface of a planet. The period of the orbit is 5800 s. The astronauts in the lander measure the diameter of the planet to be $9.60 \times 10^{6} \mathrm{~m}$. The lander sets down at the north pole of the planet. What is the weight of an $85.6 \mathrm{~kg}$ astronaut as he steps out onto the planet's surface?