View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56041U 26145.51636846 +.00000000 +00000-0 +10812-4 0 00002
2 56041 43.0017 320.1085 0001830 246.5197 113.5463 15.27584125 01
| Epoch (UTC): | 25 May 2026 12:23:34 |
| Eccentricity: | 0.0001830 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 320.1085° |
| argument of perigee: | 246.5197° |
| revolutions per day: | 15.27584125 |
| mean anomaly at epoch: | 113.5463° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|