Enabling orbit determinator to predict orbits using real time data. It will be done using 5 steps:
- Finding a set of Keplerian elements that approximate the orbit well.
- Propagate the state until new observed data is available.
- Fetch new observations.
- Refine the estimate using Kalman filter.
- Repeat steps 2 to 4.
Also, allowing orbit determinator to output the data in various ways (position, velocity or right ascension, declination or ground track or 3D plot).