For hyperbolic orbits beter use PericenterDistance then SemiMajorAxis.
Here ssc code to this comet at time close to perihelion date
Anyway I set MeanAnomaly to 2.952250395318073E-07 but 0.00 will be corect to.
Code: Select all
"C/2012 S1 (ISON)" "Sol"
{
Class "comet"
Mesh "roughsphere.cms"
Texture "asteroid.jpg"
Radius 3
EllipticalOrbit
{
Epoch 2456625.324094641844 # Epoch close to TP time and set MeanAnomaly
Period 135459.00070965014 # years
PericenterDistance 1.244362895007541E-02
Eccentricity 9.999952821752145E-01
Inclination 6.238889733909424E+01
AscendingNode 2.956547122849729E+02
ArgOfPericenter 3.455641676133329E+02
MeanAnomaly 2.952250395318073E-07
}
UniformRotation { Period 24 }
Albedo 0.04
}
I compare results with SPICE data from HORIZONS/SSD/JPL generated with telnet.