What causes orbital decay?
Orbital decay is primarily caused by atmospheric drag for low Earth orbit satellites and gravitational perturbations from the Earth, Moon, and other celestial bodies. Solar radiation pressure and the oblateness of the Earth also contribute. Over time, these factors result in the gradual reduction of an orbiting object's altitude.
How can orbital decay be mitigated?
Orbital decay can be mitigated by increasing a satellite's altitude using propulsion systems, implementing drag-reduction devices, adopting low-drag satellite designs, and periodically performing reboost manoeuvres to counteract atmospheric drag.
How does atmospheric drag affect orbital decay?
Atmospheric drag slows down a satellite by creating friction against the thin atmospheric particles present at high altitudes. This reduction in velocity decreases the satellite's orbital altitude, leading to gradual orbital decay. As the satellite descends, drag increases, further accelerating the decay process. Ultimately, the satellite may re-enter and burn up in the atmosphere.
What are the consequences of orbital decay for satellites?
Orbital decay causes satellites to lose altitude, increasing atmospheric drag and leading to eventual re-entry and disintegration or crash. This limits their operational lifespan and can contribute to space debris, posing collision risks to other space assets.
What is the difference between orbital decay and orbital degradation?
Orbital decay refers to the gradual reduction in the altitude of an object in orbit due to atmospheric drag, gravitational perturbations, and other forces. Orbital degradation, on the other hand, encompasses the overall decline in the performance or functionality of an orbiting object, including structural wear and environmental damage.