A debris retrieval system including a debris retrieval control apparatus to control retrieval of debris , the debris retrieval system comprising: a first satellite ; a second satellite ; the debris retrieval control apparatus comprising: an apparatus communication device to communicate with at least one of the first satellite and the second satellite ; a control unit to generate a control command to capture the debris , the control command controlling the first satellite and the second satellite to sandwich the debris between the first satellite and the second satellite such that the first satellite and the second satellite are both connected to the debris and carry out an active control operation during orbital descent on a flying object which is the first satellite , the debris , and the second satellite being connected together, and transmit the control command to at least one of the first satellite and the second satellite via the apparatus communication device , wherein the debris is an artificial satellite or rocket debris, the debris retrieval control apparatus is configured to communicate with at least one of the first satellite and the second satellite , each of the first satellite and the second satellite includes a capture device to capture the debris based on the control command and a propulsion device to carry out the active control operation during orbital descent on the flying object based on the control command, and the control unit is configured to transmit the control command, the control command further controlling the first satellite and the second satellite to place the first satellite and the second satellite so that a center-of-gravity position of the flying object is on a straight line of a traveling direction vector of the propulsion devices . a first satellite ; a second satellite ; the debris retrieval control apparatus comprising: an apparatus communication device to communicate with at least one of the first satellite and the second satellite ; a control unit to generate a control command to capture the debris , the control command controlling the first satellite and the second satellite to sandwich the debris between the first satellite and the second satellite such that the first satellite and the second satellite are both connected to the debris and carry out an active control operation during orbital descent on a flying object which is the first satellite , the debris , and the second satellite being connected together, and transmit the control command to at least one of the first satellite and the second satellite via the apparatus communication device , wherein the debris is an artificial satellite or rocket debris, the debris retrieval control apparatus is configured to communicate with at least one of the first satellite and the second satellite , each of the first satellite and the second satellite includes a capture device to capture the debris based on the control command and a propulsion device to carry out the active control operation during orbital descent on the flying object based on the control command, and the control unit is configured to transmit the control command, the control command further controlling the first satellite and the second satellite to place the first satellite and the second satellite so that a center-of-gravity position of the flying object is on a straight line of a traveling direction vector of the propulsion devices . <EOS>