View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 58496U 23187A 24358.23432009 .00002809 00000-0 36237-3 0 9991
2 58496 97.9715 73.1686 0013316 104.9188 255.3500 14.81757964 56944
| Epoch (UTC): | 23 December 2024 05:37:25 |
| Eccentricity: | 0.0013316 |
| inclination: | 97.9715° |
| perigee height: | 614 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 73.1686° |
| argument of perigee: | 104.9188° |
| revolutions per day: | 14.81757964 |
| mean anomaly at epoch: | 255.3500° |
| orbit number at epoch: | 5694 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|