Hi all,
In TLEPropagator, the perige
is recovered using SGP4/SDP4 theory. It can be treat as somewhat mean element (I am not sure).
Currently I need this to do a further analysis.
So I propose to add an public get method.
public double getMeanPerigee() {
return perige;
}
PS: Is that a convenient way to compute ‘mean’ orbit element from osculating orbit.