The inertia tensor of a rigid body, such as a spacecraft, can be represented as a symmetric 3x3 matrix regardless of the rotation about multiple axes (x, y, z). The elements of this tensor depend solely on the mass distribution of the body, not the axis of rotation. While a body can have angular momentum components in all three axes, it can only rotate about one specific axis at a time. When restricted to a single axis, some components of the inertia matrix become irrelevant but remain unchanged. Understanding these principles clarifies the relationship between the inertia tensor and the body's rotational dynamics.