The Gravity Recovery and Climate Experiment Follow-On (GRACE-FO) mission (Landerer et al., 2020) was successfully started on 22 May 2018, and since then, provides high-quality observations to continue the gravity field time series of its predecessor, the GRACE mission (2002( -2017( ) (Tapley et al., 2004. Similar to GRACE, both satellites in GRACE-FO mission are equipped with high precision accelerometers to measure the non-gravitational forces (e.g., atmospheric drag and radiation pressure), as well as disturbances due to satellite's operation, such as attitude thruster activation. With the aim of gravity field recovery, these measurements are essential to reduce the effects of non-gravitational perturbations from the orbit and obtain the sought-after gravitational components.Early studies have shown that the accelerometer measurements (ACC) from both GRACE-FO satellites are contaminated by different types of noise. Therefore, the standard GRACE Level-1A to Level-1B processing (Wu et al., 2006) does not deliver ACC Level-1B (ACC1B) products with sufficient accuracy for gravity field recovery. For this reason, the GRACE-FO Science Data System (SDS) team has developed specific calibration process for the accelerometer on each satellite and has provided the calibrated GRACE-FO accelerometer data (ACT) products (McCullough et al., 2019).