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Space Debris Rendezvous Analysis
· In the rendezvous analysis process, the distance between the two objects when they are closest needs to be calculated, which is called the rendezvous distance. The time to reach the shortest distance is called "rendezvous time", and the probability of collision is called "collision probability", which is used to decide whether maneuver avoidance is needed.
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Satellite Evasive Maneuver
· When confirming the risk of collision, it is necessary to use the satellite's own power to maneuver orbit to move it away from the original orbit that is in danger of collision with space debris and move to a safe orbit.
· The evaded orbit must be strictly recalculated to ensure that the new orbit will not collide with other debris.
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Satellite Orbital Control Support
· Emposat has self-developed orbit control software, and has rich experience in various satellite orbit control, and can provide technical support for satellite orbit control.
· Using the resources of the Emposat's TT&C stations at home and abroad to provide users with evasion maneuvering and emergency TT&C support.