Hodograph Representation of Almost Circular Satellite Orbits with Drag

2016 ◽  
Vol 39 (2) ◽  
pp. 390-397
Author(s):  
Mayer Humi
1962 ◽  
Vol 67 (1) ◽  
pp. 329-335 ◽  
Author(s):  
Leon Blitzer ◽  
E. M. Boughton ◽  
G. Kang ◽  
R. M. Page

The influence of air drag and the geopotential on near-circular satellite orbits, eccentricity e < 0.01, is considered. A model of the atmosphere is adopted that allows for oblateness, and in which the density behaviour approximates to the observed diurnal variation. Differential equations governing the variation in e and the argument of perigee ω are derived by combining the effects of air drag with those of the Earth’s gravitational field. These are solved numerically using initial conditions obtained from a series of computed orbits of the satellite 1963-27 A. The behaviour of the orbital elements predicted by the numerical solution is compared with the observed elements to test the developed theory, and to obtain values of atmospheric parameters at heights near 400 km.


2015 ◽  
Vol 123 (1) ◽  
pp. 85-103 ◽  
Author(s):  
Vladimir Martinusi ◽  
Lamberto Dell’Elce ◽  
Gaëtan Kerschen

AIAA Journal ◽  
1964 ◽  
Vol 2 (7) ◽  
pp. 1174-1178 ◽  
Author(s):  
F. T. GEYLING

1964 ◽  
Vol 1 (5) ◽  
pp. 513-519 ◽  
Author(s):  
J. OTTERMAN ◽  
K. LICHTENFELD

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