View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 20907U 90081BT 24279.35788610 .00149939 00000-0 13600-1 0 9994
2 20907 98.0799 312.1320 0008389 153.2918 218.4809 14.94491513782090
| Epoch (UTC): | 05 October 2024 08:35:21 |
| Eccentricity: | 0.0008389 |
| inclination: | 98.0799° |
| perigee height: | 578 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 312.1320° |
| argument of perigee: | 153.2918° |
| revolutions per day: | 14.94491513 |
| mean anomaly at epoch: | 218.4809° |
| orbit number at epoch: | 78209 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|