View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68896U 26145.58335647 +.00000000 +00000-0 -60422-1 0 00005
2 68896 97.2853 341.4216 0001960 88.2104 195.7078 15.40753639 03
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001960 |
| inclination: | 97.2853° |
| perigee height: | 443 km |
| apogee height: | 445 km |
| right ascension of ascending node: | 341.4216° |
| argument of perigee: | 88.2104° |
| revolutions per day: | 15.40753639 |
| mean anomaly at epoch: | 195.7078° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|