The problem of controlling a rotating hub-spoke tethered formation system in low Earth orbit is considered. in which microsatellites are located radially around the central spacecraft (hub) and connected to it by tethers (spokes). To analyze the dynamics of the tethered system. a mathematical model is developed in the orbital coordinate system by Lagrange method. https://macorners.shop/product-category/engraved-family-stainless-steel-keychain/