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Model 9000 Tracking Receiver, Model 9050 Drive Cabinet
Tracking algorithm performing periodic and or level triggered scans to peak up signal strength (requires beacon receiver).
Points the satellite dish using an orbital model created from previous AZ and EL step-track data (requires beacon receiver).
Automatically acquires target, peak phase align and calibrate to begin tracking with monopulse tracking receiver. Transfers to predictive model or ephemeris tracking on loss of monopulse signal.
Automated tracking based on NORAD two-line element sets
Tracking derived from Intelsat 11-element parameter sets
Track using TLE as a base model but add periodic Step Tracks to correct for offsets over time
Tracking with Intelsat model, with added Step Track to correct for offsets over time
Dedicated front-panel antenna jog controls
Points the antenna to AZ and EL angles determined by the longitudinal orbital slot
Points the antenna to user-supplied AZ, EL and POL angles
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