The largest uncertainty in orbital propagation for satellites and space debris in Low Earth Orbit (LEO) is atmospheric drag, due to thermospheric density. Space weather and space climate affect thermospheric densities on timescales ranging from hours to decades.

On the short time scale, forecasting thermospheric densities is critical to provide timely and actionable conjunction warnings to avoid satellite collisions. To address this, the UK is operationalizing the University of Birmingham’s model AENeAS, an assimilative model of the thermosphere and ionosphere to aid satellite operators.

On the longer time scale, carbon dioxide cools the upper atmosphere, as the less dense thermosphere can’t trap emitted infra-red radiation. This gradually reduces thermospheric densities at a rate of 2 to 5% per decade. As neutral densities decrease, orbital lifetimes will increase, raising the probability of a collision occurring during a satellite’s lifetime. This increases the speed of feedback loop of more collisions, more space debris, more collisions, and raises the prospect of a Kessler Syndrome at lower altitudes.