View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 28975U 87001C 22330.42258427 .00001910 00000-0 13324-2 0 9997
2 28975 82.4618 3.6898 0019452 65.1513 358.7952 13.98065356481163
| Epoch (UTC): | 26 November 2022 10:08:31 |
| Eccentricity: | 0.0019452 |
| inclination: | 82.4618° |
| perigee height: | 886 km |
| apogee height: | 914 km |
| right ascension of ascending node: | 3.6898° |
| argument of perigee: | 65.1513° |
| revolutions per day: | 13.98065356 |
| mean anomaly at epoch: | 358.7952° |
| orbit number at epoch: | 48116 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|