View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 07735U 26099.99589606 +.00000000 +00000-0 +63730-4 0 00006
2 07735 114.9758 104.1031 0054841 277.0993 82.3855 14.25582527 00
| Epoch (UTC): | 09 April 2026 23:54:05 |
| Eccentricity: | 0.0054841 |
| inclination: | 114.9758° |
| perigee height: | 767 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 104.1031° |
| argument of perigee: | 277.0993° |
| revolutions per day: | 14.25582527 |
| mean anomaly at epoch: | 82.3855° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|