View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 22566U 93016B 25131.48737642 -.00000262 00000-0 -10991-3 0 9998
2 22566 71.0049 129.8698 0008246 56.1474 304.0433 14.15253044659415
| Epoch (UTC): | 11 May 2025 11:41:49 |
| Eccentricity: | 0.0008246 |
| inclination: | 71.0049° |
| perigee height: | 835 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 129.8698° |
| argument of perigee: | 56.1474° |
| revolutions per day: | 14.15253044 |
| mean anomaly at epoch: | 304.0433° |
| orbit number at epoch: | 65941 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|