View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 32791U 08021J 22019.50986472 .00001905 00000-0 19402-3 0 9992
2 32791 97.5952 0.9916 0012306 333.5650 26.4940 14.91810604744984
| Epoch (UTC): | 19 January 2022 12:14:12 |
| Eccentricity: | 0.0012306 |
| inclination: | 97.5952° |
| perigee height: | 584 km |
| apogee height: | 601 km |
| right ascension of ascending node: | 0.9916° |
| argument of perigee: | 333.5650° |
| revolutions per day: | 14.91810604 |
| mean anomaly at epoch: | 26.4940° |
| orbit number at epoch: | 74498 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|