View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 38166U 99025ERP 24357.18608275 .00010473 00000-0 45201-2 0 9996
2 38166 99.0818 80.5666 0058787 348.3744 11.6072 14.23710942586997
| Epoch (UTC): | 22 December 2024 04:27:57 |
| Eccentricity: | 0.0058787 |
| inclination: | 99.0818° |
| perigee height: | 770 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 80.5666° |
| argument of perigee: | 348.3744° |
| revolutions per day: | 14.23710942 |
| mean anomaly at epoch: | 11.6072° |
| orbit number at epoch: | 58699 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|