A spacecraft (10) for removing space debris is disclosed. The spacecraft includes a satellite bus (100), a shield member (110) foldable on an outer side face of the satellite bus and disposed facing towards space debris to reduce a movement speed of the space debris, and a support member (120) configured to support the shield member with respect to the satellite bus, in which the shield member includes a central panel (112) configured to overlap one face of the satellite bus, a plurality of first panels (114) connected to peripheral sides of the central panel and radially extended, and a plurality of second panels (116) located between the first panels.