View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 45675U 26145.15325674 +.00000000 +00000-0 +13400-2 0 00001
2 45675 53.0467 49.3396 0004620 56.0766 304.0682 15.54237976 02
| Epoch (UTC): | 25 May 2026 03:40:41 |
| Eccentricity: | 0.0004620 |
| inclination: | 53.0467° |
| perigee height: | 401 km |
| apogee height: | 408 km |
| right ascension of ascending node: | 49.3396° |
| argument of perigee: | 56.0766° |
| revolutions per day: | 15.54237976 |
| mean anomaly at epoch: | 304.0682° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|