View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 20U 59007A 23337.11751720 .00001074 00000-0 43425-3 0 9998
2 20 33.3450 355.2226 1656499 137.5729 236.5551 11.57985230376948
| Epoch (UTC): | 03 December 2023 02:49:13 |
| Eccentricity: | 0.1656499 |
| inclination: | 33.3450° |
| perigee height: | 507 km |
| apogee height: | 3241 km |
| right ascension of ascending node: | 355.2226° |
| argument of perigee: | 137.5729° |
| revolutions per day: | 11.57985230 |
| mean anomaly at epoch: | 236.5551° |
| orbit number at epoch: | 37694 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|