An improved solar power station comprising: - at least one solar device configured to generate power from solar energy; - at least one space lattice configuration having framework members interconnected at their ends in a pattern that consists of at least one semi-cuboctahedron (1⁄2 CO ) and at least one semi-octahedron (1⁄2 O ); - at least one foundation having a bearing plane ; wherein: - said solar device is connected to said space lattice configuration ; - said space lattice configuration is configured to rotate, with respect to said foundation , about just one axis which is perpendicular to said bearing plane ; - said foundation comprises a ring , said bearing plane comprising the top of said ring ; characterized in that: - said foundation further comprises a central hub , at least three pre-tensioned spokes radiating from said hub , at least three helical piles , wherein said hub is fixed to said spokes , said spokes are connected to said ring , said ring is fixed to said piles , and wherein said spokes are configured to restrain said hub with respect to said ring , said spokes comprising pre-tensioning means so as to enable pre-tensioning, said pre-tensioning means further comprising radial distance regulating means ; - said space lattice configuration is rotatably mounted to said hub in a manner that allows rotation with respect to said foundation , said axis passing through the centre of said hub ; - said solar power station further comprises at least one restraining device , wherein said restraining device comprises a structural bearing configured to restrain said space lattice configuration with respect to said ring when actuated, in a manner that said space lattice configuration acquires structural integrity and becomes a space lattice structure , and wherein said restraining device is fixed to said space lattice configuration , bears on said bearing plane , and is connected to said ring . - at least one solar device configured to generate power from solar energy; - at least one space lattice configuration having framework members interconnected at their ends in a pattern that consists of at least one semi-cuboctahedron (1⁄2 CO ) and at least one semi-octahedron (1⁄2 O ); - at least one foundation having a bearing plane ; wherein: - said solar device is connected to said space lattice configuration ; - said space lattice configuration is configured to rotate, with respect to said foundation , about just one axis which is perpendicular to said bearing plane ; - said foundation comprises a ring , said bearing plane comprising the top of said ring ; - said foundation further comprises a central hub , at least three pre-tensioned spokes radiating from said hub , at least three helical piles , wherein said hub is fixed to said spokes , said spokes are connected to said ring , said ring is fixed to said piles , and wherein said spokes are configured to restrain said hub with respect to said ring , said spokes comprising pre-tensioning means so as to enable pre-tensioning, said pre-tensioning means further comprising radial distance regulating means ; - said space lattice configuration is rotatably mounted to said hub in a manner that allows rotation with respect to said foundation , said axis passing through the centre of said hub ; - said solar power station further comprises at least one restraining device , wherein said restraining device comprises a structural bearing configured to restrain said space lattice configuration with respect to said ring when actuated, in a manner that said space lattice configuration acquires structural integrity and becomes a space lattice structure , and wherein said restraining device is fixed to said space lattice configuration , bears on said bearing plane , and is connected to said ring . <EOS>