View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 22804U 93059C 24357.86906486 .00000355 00000-0 37503-3 0 9994
2 22804 70.9722 164.9325 0209792 184.6786 284.2024 13.71867797564535
| Epoch (UTC): | 22 December 2024 20:51:27 |
| Eccentricity: | 0.0209792 |
| inclination: | 70.9722° |
| perigee height: | 838 km |
| apogee height: | 1147 km |
| right ascension of ascending node: | 164.9325° |
| argument of perigee: | 184.6786° |
| revolutions per day: | 13.71867797 |
| mean anomaly at epoch: | 284.2024° |
| orbit number at epoch: | 56453 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|