View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68775U 26145.58335647 +.00000000 +00000-0 -27379-1 0 00005
2 68775 97.2847 182.4279 0001488 82.3686 26.8820 15.58496139 06
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001488 |
| inclination: | 97.2847° |
| perigee height: | 391 km |
| apogee height: | 393 km |
| right ascension of ascending node: | 182.4279° |
| argument of perigee: | 82.3686° |
| revolutions per day: | 15.58496139 |
| mean anomaly at epoch: | 26.8820° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|