Abstract An approximate technique for calculating the satellite orbit decay under the aerodynamic drag effect for arbitrary values of the orbit eccentricity and for the realistic model of the altitude dependence of the atmospheric density is proposed.
Estimation of a Satellite Lifetime in Orbit
Cosmic Research ; 39 , 3 ; 266-274
2001-05-01
9 pages
Article (Journal)
Electronic Resource
English
Estimation of a Satellite Lifetime in Orbit
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