View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 27431U 02024B 24349.40460294 .00000203 00000-0 14037-3 0 9999
2 27431 99.0325 28.9035 0015199 351.7888 8.3031 14.10081429162069
| Epoch (UTC): | 14 December 2024 09:42:37 |
| Eccentricity: | 0.0015199 |
| inclination: | 99.0325° |
| perigee height: | 848 km |
| apogee height: | 870 km |
| right ascension of ascending node: | 28.9035° |
| argument of perigee: | 351.7888° |
| revolutions per day: | 14.10081429 |
| mean anomaly at epoch: | 8.3031° |
| orbit number at epoch: | 16206 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|