View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 8520U 75124B 24255.01017478 .00000166 00000-0 87949-4 0 9994
2 8520 81.2868 132.8444 0027370 69.0504 291.3592 14.09243694503370
| Epoch (UTC): | 11 September 2024 00:14:39 |
| Eccentricity: | 0.0027370 |
| inclination: | 81.2868° |
| perigee height: | 842 km |
| apogee height: | 882 km |
| right ascension of ascending node: | 132.8444° |
| argument of perigee: | 69.0504° |
| revolutions per day: | 14.09243694 |
| mean anomaly at epoch: | 291.3592° |
| orbit number at epoch: | 50337 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|