View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 01953U 66005B 24357.87432248 .00000329 00000-0 33336-3 0 9999
2 01953 90.1524 344.2234 0227317 351.1108 8.6054 13.64910515929035
| Epoch (UTC): | 22 December 2024 20:59:01 |
| Eccentricity: | 0.0227317 |
| inclination: | 90.1524° |
| perigee height: | 850 km |
| apogee height: | 1186 km |
| right ascension of ascending node: | 344.2234° |
| argument of perigee: | 351.1108° |
| revolutions per day: | 13.64910515 |
| mean anomaly at epoch: | 8.6054° |
| orbit number at epoch: | 92903 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|