| CPC B64G 1/283 (2013.01) [B64G 1/244 (2019.05)] | 20 Claims |

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1. A spacecraft comprising:
an antenna element;
one or more wheels each configured to provide torque to the antenna element, wherein each wheel of the one or more wheels is aligned with at least two planes of a three-dimensional plane relative to the spacecraft; and
one or more processors configured to control operating modes of the one or more wheels by changing windings of the one or more wheels, wherein the operating modes comprise a first operating mode that provides a first amount of torque to the antenna element and a second operating mode that provides a second amount of torque to the antenna element greater than the first amount of torque.
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