Calculating the weight of celestial bodies in the solar system primarily involves observing the acceleration of objects as they approach a planet, which reveals the gravitational pull related to its mass. Kepler's 3rd Law is essential for this calculation, expressed as M = (4pi^2/G)(d^3/T^2), where M is the mass of the planet, d is the orbital radius, and T is the orbital period of a satellite. This method can be applied universally, allowing for the determination of the sun's mass using a planet's orbit or Earth's mass through a satellite's orbit. Additionally, once the mass is known, the size can be observed to compute density and infer composition. These calculations are foundational in celestial mechanics and can be adapted for eccentric orbits.