View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 32791U 08021J 24286.49815604 .00019382 00000-0 12515-2 0 9991
2 32791 97.7036 257.4024 0001721 277.2162 82.8870 15.08292198894254
| Epoch (UTC): | 12 October 2024 11:57:20 |
| Eccentricity: | 0.0001721 |
| inclination: | 97.7036° |
| perigee height: | 540 km |
| apogee height: | 542 km |
| right ascension of ascending node: | 257.4024° |
| argument of perigee: | 277.2162° |
| revolutions per day: | 15.08292198 |
| mean anomaly at epoch: | 82.8870° |
| orbit number at epoch: | 89425 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|