## The Drift of a 24-hour Equatorial Satellite Due to an Earth Gravity Field Through 4th Order, Volume 2103 |

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24-HOUR EQUATORIAL SATELLITE 24-hour satellite 4th order acceleration Appendix approximate assumed become character characteristic solutions coefficients constants coordinates damped determined dimensionless dominant drift drift Equations drift motion dynamically EARTH GRAVITY FIELD earth's equator Equa Equation 48 Equation 57 Equation 61 FIELD THROUGH 4th Figure four geographic longitude geopotential Greenwich harmonic ignoring inertial initial perturbation injection Kozai latitude perturbation linear system longitude perturbation magnitude Major Axis maximum minor axis motion NASA TN noted numerical integration oblate orbit oscillation percent perfect injection period perturbation force perturbation rates potential predicted Private Communication radial perturbation forces radii rates Reference report extends previous respect self-limiting sidereal days sin2 solutions to Equation Solve spherical stable regions statute miles synchronous radius synchronous satellite tion triaxial triaxial field turbation uncoupled vicinity Wagner zero zero initial