![]() If one or more of the conditions are not satisfied, in addition to fuel which is used to guarantee normal in-orbit maintenance or a preset orbit transfer mission, a maximum deviation, which can be corrected by the semi-major axis, the tilt angle, and the eccentricity, can be estimated according to a fuel allowance and all values are weighted and added, and the satellite injection result is a "success" when a sum of all the values is less than 1. Orbit quantities including a semi-major axis deviation |delta a|, a tilt angle deviation |delta i|, and an eccentricity deviation |delta e| in satellite injection are used to determine whether maximum deviation of |delta aL|, |delta iL| and |delta eL| given by a carrier rocket are met and if all the maximum deviation are met, the satellite injection result is "a complete success".
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