View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56015U 26145.55220264 +.00000000 +00000-0 +42274-4 0 00007
2 56015 43.0043 330.8973 0001429 266.0249 94.0439 15.27572519 04
| Epoch (UTC): | 25 May 2026 13:15:10 |
| Eccentricity: | 0.0001429 |
| inclination: | 43.0043° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 330.8973° |
| argument of perigee: | 266.0249° |
| revolutions per day: | 15.27572519 |
| mean anomaly at epoch: | 94.0439° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|