View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68106U 26145.37872160 +.00000000 +00000-0 +90481-3 0 00001
2 68106 97.2858 105.9692 0002121 114.3170 245.8294 15.33454464 00
| Epoch (UTC): | 25 May 2026 09:05:21 |
| Eccentricity: | 0.0002121 |
| inclination: | 97.2858° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 105.9692° |
| argument of perigee: | 114.3170° |
| revolutions per day: | 15.33454464 |
| mean anomaly at epoch: | 245.8294° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|