View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00050U 60009B 23339.86313857 -.00000023 00000-0 59419-3 0 9998
2 00050 47.2277 150.7130 0113833 139.9069 221.0188 12.20136093824844
| Epoch (UTC): | 05 December 2023 20:42:55 |
| Eccentricity: | 0.0113833 |
| inclination: | 47.2277° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 150.7130° |
| argument of perigee: | 139.9069° |
| revolutions per day: | 12.20136093 |
| mean anomaly at epoch: | 221.0188° |
| orbit number at epoch: | 82484 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|