View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00012U 59001B 22022.50382764 .00000760 00000-0 42726-3 0 9998
2 00012 32.9118 107.2978 1665924 266.9559 74.0006 11.44504080346892
| Epoch (UTC): | 22 January 2022 12:05:30 |
| Eccentricity: | 0.1665924 |
| inclination: | 32.9118° |
| perigee height: | 553 km |
| apogee height: | 3325 km |
| right ascension of ascending node: | 107.2978° |
| argument of perigee: | 266.9559° |
| revolutions per day: | 11.44504080 |
| mean anomaly at epoch: | 74.0006° |
| orbit number at epoch: | 34689 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|