View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 30741U 99025ATB 24357.00930854 .00000487 00000-0 28465-3 0 9997
2 30741 98.6924 10.7616 0007083 59.9889 329.5736 14.12922947917959
| Epoch (UTC): | 22 December 2024 00:13:24 |
| Eccentricity: | 0.0007083 |
| inclination: | 98.6924° |
| perigee height: | 844 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 10.7616° |
| argument of perigee: | 59.9889° |
| revolutions per day: | 14.12922947 |
| mean anomaly at epoch: | 329.5736° |
| orbit number at epoch: | 91795 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|