View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 26931U 01043C 22342.37547742 .00000168 00000-0 95567-4 0 9992
2 26931 67.0514 329.4554 0005241 271.4572 88.5929 14.30772619106286
| Epoch (UTC): | 08 December 2022 09:00:41 |
| Eccentricity: | 0.0005241 |
| inclination: | 67.0514° |
| perigee height: | 785 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 329.4554° |
| argument of perigee: | 271.4572° |
| revolutions per day: | 14.30772619 |
| mean anomaly at epoch: | 88.5929° |
| orbit number at epoch: | 10628 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|