So it is more likely that given average orbital speed and average orbital distance the we have a good estimate of the planet mass, by calculating centripetal force, Fm
Oavg = ( aphelion + perihelion )/2 = ( 249 209 300 +206669000 )/2 = 227939150 km
Fm=V2avgOavg = ((24.077)^2)/227939150 = 0.00000254 kms-2
And we move on to orbital speed at the aphelion,
(249 209 300*0.00000254 )^(0.5) = 25.15 kms-1
Orbital speed at the perihelion,
(206 669 000*0.00000254 )^(0.5) = 22.91 kms-1
And the orbital speed from considering △GPE alone is,
v=√3gmrm = (3*0.003711*3390 )^(0.5) = 6.143 kms-1
The actual Mars orbital speed is measured as 24.077 kms-1
In a similar way based on the model for Earth where the final orbital velocity is the sum of two rotating velocities, Vm1 and Vm2, and Mars has a initial velocity Vi when it was captured by the Sun,
Vm1−Vm2 = 25.15 kms-1
Vm1+Vm2 = 22.91 kms-1
Vm1 = ( 25.15 + 22.91 )/2 = 24.03 kms-1 and
Vm2 = 25.15 - 24.03 = 1.12 kms-1
The parallel component of the final orbiting velocity is the sum of the velocity the body would have considering a decrease in GPE alone and the parallel component of the initial approach velocity. To find the parallel initial velocity component,
Vm1 = √2∗△GPE+Vip = 6.143 + Vip = 24.03 kms-1
Vip = 24.03-6.143 = 17.89 kms-1
The second smaller rotating velocity is the perpendicular component of the initial velocity, Vi.
Vir = 1.12 kms-1
Vi=√V2ip+V2ir = ((1.12)^2 + (17.89)^2)^(0.5) = 17.92 kms-1
So, Mars approached the Sun with an initial velocity Vi = 17.92 kms-1 and was captured by the Sun.