View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56900U 26145.57990171 +.00000000 +00000-0 +36622-4 0 00003
2 56900 43.0061 356.7849 0001603 272.7032 87.3637 15.27578485 07
| Epoch (UTC): | 25 May 2026 13:55:03 |
| Eccentricity: | 0.0001603 |
| inclination: | 43.0061° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 356.7849° |
| argument of perigee: | 272.7032° |
| revolutions per day: | 15.27578485 |
| mean anomaly at epoch: | 87.3637° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|