An acceleration-measuring method by a satellite receiver carrier tracking loop comprises a step (1) that a radio-frequency signal received by an antenna is converted into a data medium-frequency signal through a radio-frequency front end processing chip, a step (2) that signal capture is achieved by adoption of a frequency domain parallel acquisition method, a step (3) that carrier tracking is achieved through adoption of a third-order phase locked loop and pseudorandom code tracking is achieved through a delay locked loop, a step (4) that after carrier peeling and pseudorandom code peeling of the data medium-frequency signal are achieved through baseband signal processing, navigation data are obtained, the navigation data are decoded to get a satellite ephemeris, and acceleration of the satellite is calculated by the usage of information difference of satellite speed, a step (5) that an acceleration state parameter in a carrier loop wave filter is sent out, and line-of-sight acceleration relative to the tracked satellite of a user is obtained after sacel transformation of a fixed scale transformation ka, and a step (6) that the acceleration of the receiver is calculated. The acceleration-measuring method by the satellite receiver carrier tracking loop has the advantages of being simple in principle, high in measuring precision, wide in application range and the like.