View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68845U 26145.58335647 +.00000000 +00000-0 +31029-3 0 00001
2 68845 97.2849 160.2929 0001254 95.2040 162.2805 15.49175225 08
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001254 |
| inclination: | 97.2849° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 160.2929° |
| argument of perigee: | 95.2040° |
| revolutions per day: | 15.49175225 |
| mean anomaly at epoch: | 162.2805° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|