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 23265.90765141 .00009311 00000-0 79206-3 0 9995
2 32791 97.6656 235.2251 0013133 84.6999 275.5722 14.97975383836282
| Epoch (UTC): | 22 September 2023 21:47:01 |
| Eccentricity: | 0.0013133 |
| inclination: | 97.6656° |
| perigee height: | 564 km |
| apogee height: | 582 km |
| right ascension of ascending node: | 235.2251° |
| argument of perigee: | 84.6999° |
| revolutions per day: | 14.97975383 |
| mean anomaly at epoch: | 275.5722° |
| orbit number at epoch: | 83628 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|