View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 28522U 05002B 24257.83991889 .00000290 00000-0 22142-3 0 9996
2 28522 82.9484 148.8888 0044008 266.3876 93.2255 13.89881797996556
| Epoch (UTC): | 13 September 2024 20:09:28 |
| Eccentricity: | 0.0044008 |
| inclination: | 82.9484° |
| perigee height: | 897 km |
| apogee height: | 961 km |
| right ascension of ascending node: | 148.8888° |
| argument of perigee: | 266.3876° |
| revolutions per day: | 13.89881797 |
| mean anomaly at epoch: | 93.2255° |
| orbit number at epoch: | 99655 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|