View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53905U 26145.54077928 +.00000000 +00000-0 +49211-5 0 00007
2 53905 53.2113 329.3439 0001107 84.9936 275.1182 15.08833855 02
| Epoch (UTC): | 25 May 2026 12:58:43 |
| Eccentricity: | 0.0001107 |
| inclination: | 53.2113° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 329.3439° |
| argument of perigee: | 84.9936° |
| revolutions per day: | 15.08833855 |
| mean anomaly at epoch: | 275.1182° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|