View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 53106U 22080B 22354.08419093 -.00000003 00000-0 00000 0 0 9990
2 53106 70.1702 21.9397 0008914 226.9685 182.2049 6.42557326 10248
| Epoch (UTC): | 20 December 2022 02:01:14 |
| Eccentricity: | 0.0008914 |
| inclination: | 70.1702° |
| perigee height: | 5832 km |
| apogee height: | 5854 km |
| right ascension of ascending node: | 21.9397° |
| argument of perigee: | 226.9685° |
| revolutions per day: | 6.42557326 |
| mean anomaly at epoch: | 182.2049° |
| orbit number at epoch: | 1024 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|