View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 09904U 77024B 25198.37385677 -.00000055 00000-0 -39551-4 0 9992
2 09904 81.2642 156.7756 0051855 292.4342 67.1340 14.07264158477696
| Epoch (UTC): | 17 July 2025 08:58:21 |
| Eccentricity: | 0.0051855 |
| inclination: | 81.2642° |
| perigee height: | 831 km |
| apogee height: | 906 km |
| right ascension of ascending node: | 156.7756° |
| argument of perigee: | 292.4342° |
| revolutions per day: | 14.07264158 |
| mean anomaly at epoch: | 67.1340° |
| orbit number at epoch: | 47769 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|