View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56028U 26145.49966784 +.00000000 +00000-0 -21636-4 0 00008
2 56028 43.0036 331.3468 0001652 264.6019 95.4645 15.27582996 06
| Epoch (UTC): | 25 May 2026 11:59:31 |
| Eccentricity: | 0.0001652 |
| inclination: | 43.0036° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 331.3468° |
| argument of perigee: | 264.6019° |
| revolutions per day: | 15.27582996 |
| mean anomaly at epoch: | 95.4645° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|