The analytic Keplerian 6 X 6 Earth Centered Inertial state transition
matrix developed by Goodyear, Battin, and other mathematicians is well
known. The primary objectives of this paper are to present a relative
ly simple formulation of the Keplerian state transition matrix, and to
show that the higher-order secular terms associated with the state tr
ansition matrices of Goodyear and Battin can be eliminated. Analytic a
nd numerical results indicate that the concern about these unbounded s
ecular terms for numerical integration is not warranted. Comparison of
Keplerian, Vinti, and numerical state transition matrices in the Hill
-Clohessy-Wiltshire coordinate system (local-vertical coordinate syste
m) further supports this contention since the two secular elements of
the Keplerian state transition matrix match closely with those of the
Vinti and numerical state transition matrices.