SYS_EXTRACTION_INIT
DOWNLINKING VECTOR PARAMETERS
DECRYPTING CORE ALGORITHMS...
DECRYPTING CORE ALGORITHMS...
Audit the drag. Estimate the remaining orbital lifetime of a satellite in Low Earth Orbit (LEO) due to atmospheric drag.
At 400 km, the atmosphere is thin but still present. With Medium solar activity (which expands the atmosphere), your satellite will likely re-enter the atmosphere in approximately 0.7 years. Regular station-keeping burns are required to counter this decay and maintain orbit.