View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52770U 22057AQ 25269.24431773 .16420677 37577-5 24958-3 0 9990
2 52770 97.5905 64.5687 0014057 267.2240 92.7453 16.47667105186619
| Epoch (UTC): | 26 September 2025 05:51:49 |
| Eccentricity: | 0.0014057 |
| inclination: | 97.5905° |
| perigee height: | 136 km |
| apogee height: | 154 km |
| right ascension of ascending node: | 64.5687° |
| argument of perigee: | 267.2240° |
| revolutions per day: | 16.47667105 |
| mean anomaly at epoch: | 92.7453° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|