View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 31805U 99025CGT 24355.78910137 .00009673 00000-0 27356-2 0 9997
2 31805 98.3535 3.8118 0478650 87.1340 278.4483 13.94973715573725
| Epoch (UTC): | 20 December 2024 18:56:18 |
| Eccentricity: | 0.0478650 |
| inclination: | 98.3535° |
| perigee height: | 562 km |
| apogee height: | 1260 km |
| right ascension of ascending node: | 3.8118° |
| argument of perigee: | 87.1340° |
| revolutions per day: | 13.94973715 |
| mean anomaly at epoch: | 278.4483° |
| orbit number at epoch: | 57372 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|