| Section | Element | Value |
|---|---|---|
| Shape of a Satellite | Mass | 8,500 kg |
| Reflection Area | 17 m2 | |
| Drag Area | 17 m2 | |
| Drag Coefficient | 2.2 | |
| Reflectivity Coefficient | 1.2 | |
| Initial Orbit condition | Semi-major axis Altitude | 6,699.4 km |
| Eccentricity | 0.002055 | |
| Orbital Inclination | 42.80° | |
| The Right Ascension of Ascending Node | 28.13° | |
| Argument of Perigee | 332.87° | |
| Mean Anomaly | 182.50° | |
| Initial Time (UTC) | Date | 2017-09-11 |
| Time | 18:18:31 | |