View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 21805U 91080B 23339.69730427 -.00000054 00000-0 00000+0 0 9991
2 21805 14.5069 352.1815 0004853 100.4427 253.2055 0.99188585 16536
| Epoch (UTC): | 05 December 2023 16:44:07 |
| Eccentricity: | 0.0004853 |
| inclination: | 14.5069° |
| perigee height: | 36072 km |
| apogee height: | 36113 km |
| right ascension of ascending node: | 352.1815° |
| argument of perigee: | 100.4427° |
| revolutions per day: | 0.99188585 |
| mean anomaly at epoch: | 253.2055° |
| orbit number at epoch: | 1653 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|