General planetary geospatial transportation complex, comprising a general planetary vehicle encircling the planet along the line of the planet surface cross-section by the plane parallel to the plane of the equator, said complex fastened on launch overpass of altitude h, m, defined by the ratio: 10 − 7 ≤ h / R ≤ 10 − 4, where R, is the radius of the planet, said complex representing a linear bearing structure encircling the planet and having length L 0, said complex comprising a pressure hull with at least two vacuum channels, forming rings around the planet, in the first one of which a first endless planet-encircling linear flywheel (10.1) is located, and in the second one a second endless planet-encircling linear flywheel (10.2) is located, wherein the first linear flywheel (10.1) and the second linear flywheel (10.2) are contactlessly positioned in relation to the walls of the corresponding vacuum channels and equipped with systems (11, 12) of magnetic and/or electromagnetic suspension and linear electromagnetic drives respectively, configured to accelerate the linear flywheels (10.1, 10.2) to velocity V 0, m/s defined by the ratio: 1,1 ≤ V 0 / V eh ≤ 5, where V eh, is the first cosmic velocity at altitude h, the linear bearing structure is equipped with transportation compartments and configured to be elongated without uniformity loss, defined by the ratio: 1,01 ≤ L H / L 0 ≤ 1,25, where L H, is the length of the linear bearing structure at circular orbit of altitude H, and linear flywheels (10.1, 10.2) having masses m 1 and m 2, defined by the ratio: 0,1 ≤ m 1 / m 2 ≤ 10, wherein the drives of linear flywheels (10.1, 10.2) are connected with power supply source via control and communication systems (17, 18); wherein the general planetary geospatial transportation complex is equipped with fixing locks at launch altitude h, along the entire length L 0. where R, is the radius of the planet, said complex representing a linear bearing structure encircling the planet and having length L 0, said complex comprising a pressure hull with at least two vacuum channels, forming rings around the planet, in the first one of which a first endless planet-encircling linear flywheel (10.1) is located, and in the second one a second endless planet-encircling linear flywheel (10.2) is located, wherein the first linear flywheel (10.1) and the second linear flywheel (10.2) are contactlessly positioned in relation to the walls of the corresponding vacuum channels and equipped with systems (11, 12) of magnetic and/or electromagnetic suspension and linear electromagnetic drives respectively, configured to accelerate the linear flywheels (10.1, 10.2) to velocity V 0, m/s defined by the ratio: 1,1 ≤ V 0 / V eh ≤ 5, where V eh, is the first cosmic velocity at altitude h, the linear bearing structure is equipped with transportation compartments and configured to be elongated without uniformity loss, defined by the ratio: 1,01 ≤ L H / L 0 ≤ 1,25, where L H, is the length of the linear bearing structure at circular orbit of altitude H, and linear flywheels (10.1, 10.2) having masses m 1 and m 2, defined by the ratio: 0,1 ≤ m 1 / m 2 ≤ 10, wherein the drives of linear flywheels (10.1, 10.2) are connected with power supply source via control and communication systems (17, 18); wherein the general planetary geospatial transportation complex is equipped with fixing locks at launch altitude h, along the entire length L 0.