View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 21666U 91059A 23268.74640491 .00000078 00000-0 67128-4 0 9994
2 21666 82.9049 128.6291 0026321 99.2969 331.3547 13.73400279608198
| Epoch (UTC): | 25 September 2023 17:54:49 |
| Eccentricity: | 0.0026321 |
| inclination: | 82.9049° |
| perigee height: | 968 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 128.6291° |
| argument of perigee: | 99.2969° |
| revolutions per day: | 13.73400279 |
| mean anomaly at epoch: | 331.3547° |
| orbit number at epoch: | 60819 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|