The motion of a satellite under the influence of the longitude-dependent terms of the geopotential is examined in a frame of reference rotating with the mean motion of the satellite. The orbits are assumed to be near-circular but unrestricted with respect to inclination. In general the effect of the tesseral harmonics is to induce short-period perturbations of small amplitude. Under special conditions, however—when the satellite's mean motion is commensurable with the earth's rotation—two distinct types of resonance may be set up. The physical behavior, as well as the mathematical description, of the motion is inherently different in the separate resonances. Specifically, dynamical resonances occur when the impressed frequency due to some Jnm term is equal to the natural frequency of the satellite's orbital motion. In this case the amplitude of the induced oscillation builds up with time, the eccentricity increases, and the orbit is unstable in the sense that it will be driven out of the resonance state. For other commensurabilities librational resonances occur when the satellite is in a localized potential well in the moving frame. In this situation the periodic motion of the satellite in the potential trough is analogous to pendulum motion. In turn, this manifests itself as a long-period libration in longitude of the satellite's ground track. For near-equatorial motion, only the 24-hour orbit is librational; the orbits in dynamical resonance are confined to the range from 12 to 48 hours, clustering around but not including the 24-hour orbit.