View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 43188U 18014J 22279.64106647 .00003633 00000-0 31005-3 0 9991
2 43188 97.6478 183.2312 0009076 290.5295 69.4954 14.98285579255569
| Epoch (UTC): | 06 October 2022 15:23:08 |
| Eccentricity: | 0.0009076 |
| inclination: | 97.6478° |
| perigee height: | 566 km |
| apogee height: | 578 km |
| right ascension of ascending node: | 183.2312° |
| argument of perigee: | 290.5295° |
| revolutions per day: | 14.98285579 |
| mean anomaly at epoch: | 69.4954° |
| orbit number at epoch: | 25556 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|