I have been recently acquainted with orbital mechanics and am trying to do some analysis on the subject. Since I don't have subject matter expertise, I was at a crossroads with trying to decide that how would one determine if a satellite has performed maneuver/rendezvous operation given the historical TLE data of that satellite from which we extract the orbital elements. To drill down further, I am approaching to the problem like this:
- I take my satellite of interest and collect the historical TLE data for it.
- Once, I have the data, I extract and calculate all the orbital parameters from the TLE.
- From the list of orbital parameters, I choose a subset of those parameters and calculate long term standardized anomalies for each of them.
- Once I have the anomalies, I filter out those dates where any one parameter has anomalies greater than 1.5 or less than -1.5.
But the deal is, I am not too sure of my subset. As of now, I have Inclination, RAAN, Argument of Perigee and Longitude.
Is there any other factor that I should add or remove from this subset in order to nail this analysis the right way? Or is there altogether any other approach that I can use?
What I'm interested in, is to find out the days when a satellite has performed maneuvers.