View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 18562U 87080H 24357.72961109 .00000338 00000-0 55594-3 0 9996
2 18562 89.9190 159.0404 0178075 254.2583 237.0950 13.39826506818297
| Epoch (UTC): | 22 December 2024 17:30:38 |
| Eccentricity: | 0.0178075 |
| inclination: | 89.9190° |
| perigee height: | 976 km |
| apogee height: | 1243 km |
| right ascension of ascending node: | 159.0404° |
| argument of perigee: | 254.2583° |
| revolutions per day: | 13.39826506 |
| mean anomaly at epoch: | 237.0950° |
| orbit number at epoch: | 81829 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|