Re-entry predictions change constantly because the atmosphere they model is constantly changing. Solar activity, object attitude, and ballistic coefficient all introduce uncertainty that compounds over time.
Re-entry predictions change constantly because the atmosphere they model is constantly changing. Solar activity, object attitude, and ballistic coefficient all introduce uncertainty that compounds over time.
The upper atmosphere expands and contracts with solar activity on timescales of hours to years.
A tumbling satellite presents a different cross-sectional area with each rotation — making drag fundamentally variable.
The ballistic coefficient (β = mass / (Cd × Area)) determines how quickly an object slows in the atmosphere.
When a re-entry window shifts by 12 hours, that's the model incorporating new atmospheric density measurements and updated solar flux data. It means the system is working correctly.