View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68906U 26145.58335647 +.00000000 +00000-0 -60648-1 0 00007
2 68906 97.2852 341.3488 0001810 69.9004 43.2815 15.41814301 04
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001810 |
| inclination: | 97.2852° |
| perigee height: | 440 km |
| apogee height: | 442 km |
| right ascension of ascending node: | 341.3488° |
| argument of perigee: | 69.9004° |
| revolutions per day: | 15.41814301 |
| mean anomaly at epoch: | 43.2815° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|