Sensitivity threshold development

[apostop1]

I am trying to develop a sensitivity analysis tool and I would appreciate it if anyone had any information on how does the error in the semimajor axis and/or other orbital elements of the orbit of a LEO satellite influence the error in pitch, yaw and roll angles?

 

[Illmatic1]

The error in the orbit elements of a Low Earth Orbit (LEO) satellite will influence the error in its pitch, yaw and roll angles. In general, the more stable the orbital elements, the less likely the satellite's attitude will be affected by disturbances. This means that any error in the orbital elements will have an effect on the attitude of the satellite. The most significant errors that can occur are those related to the semimajor axis, eccentricity, inclination and longitude of the ascending node. Errors in the semimajor axis will cause changes in the altitude, which in turn will affect the attitude of the satellite. Similarly, errors in the eccentricity, inclination and longitude of the ascending node can cause changes in the speed and direction of the satellite, which can also affect its attitude.