View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00022U 59009A 24357.81759962 .00013413 00000-0 66329-3 0 9996
2 00022 50.2749 226.9262 0102316 127.3492 233.6837 15.13573692717912
| Epoch (UTC): | 22 December 2024 19:37:20 |
| Eccentricity: | 0.0102316 |
| inclination: | 50.2749° |
| perigee height: | 454 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 226.9262° |
| argument of perigee: | 127.3492° |
| revolutions per day: | 15.13573692 |
| mean anomaly at epoch: | 233.6837° |
| orbit number at epoch: | 71791 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|