To find the radius of the orbit of Mars, we can use the equation T^2 = (4π^2 / G(M)) * r^3, where T is the orbital period, G is the gravitational constant, M is the mass of the sun, and r is the orbital radius.
Plugging in the given values:
(2.46 years)^2 = (4π^2 / 6.672 * 10^-11 Nm^2/kg^2) * r^3
r = ((2.46 years)^2 * (6.672 * 10^-11 Nm^2/kg^2)) / (4π^2) * (1.989 * 10^30 kg)^(1/3)
To find the orbital speed of Mars, we can use the equation v = 2πr / T, where v is the orbital speed, r is the orbital radius, and T is the orbital period.
Plugging in the given values:
v = 2π * r / (2.46 years)
Note: You should convert 2.46 years to seconds using year to seconds conversion factor.