A typical spacecraft tracking run consist of downloading current NORAD Two Line elements (TLE) from a few sources such as Celestrak, Space-Track and Mike McCants repository which includes classified Artsat TLE. After updating the TLE in all software being used Target selection is the next step.
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Normal mount calibration and camera cooling would be done at this point. Checking the Global Positioning System (GPS) almanac updates and ensuring a GPS signal lock and solution for accurate time is next. Performing Telescope focusing and taking camera calibration frames if necessary is next. After calibrations are done we can slew the scope to an area close to the satellite pass Acquisition of Signal (AOG) and perform a plate solve-sync to check and refine position errors.
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Next I slew to the predicated pass position and await AOG. The mount is configured to slew or "leapfrog" ahead of the pass while the camera takes exposers. When the signal is lost in the field of view the mount will again slew "leapFrog" ahead of the satellite and await the acquisition of signal again. This "leapfrog process will continue until stopped manually or the signal goes below my set parameters such as air mass settings. When imaging a Geostationary satellite the mount would slew to acquire the signal and tracking would be turned off to keep the target centered. The pass timing can be off considerably ahead or behind the predicted time due to old Elemental Set (Elset)s or atmospheric drag.
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Later, these images can be used to measure the satellites position based on the star field using a star catalogue. This is called astrometry. After the data is reduced the measurements are converted to a format such as IOD and shared to be used in generating a new TLE.
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Satellite Tracking Examples from MEO
Live satellite tracking below