Why is Period needed for Kepler inputs
Posted: 19.05.2020, 13:44
Why is the orbital period needed for Kepler inputs? Our simulation determines the orbital speed around the moon as a function of radius from the moon. I comented out the period and the vehicle did not initialize properly. Is there a way to have Celestia's velocity use the radius from the moon?
EllipticalOrbit {
#Period 0.064176392
SemiMajorAxis 3999.90
Eccentricity 0.00005
Inclination 29.999
AscendingNode 343.1518
ArgOfPericenter 346.2476
MeanAnomaly 13.8216
Epoch 2451545.0
}
EllipticalOrbit {
#Period 0.064176392
SemiMajorAxis 3999.90
Eccentricity 0.00005
Inclination 29.999
AscendingNode 343.1518
ArgOfPericenter 346.2476
MeanAnomaly 13.8216
Epoch 2451545.0
}