View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58600U 26145.25472448 +.00000000 +00000-0 +97727-4 0 00002
2 58600 43.0043 96.1819 0001522 270.0919 89.9758 15.27564770 07
| Epoch (UTC): | 25 May 2026 06:06:48 |
| Eccentricity: | 0.0001522 |
| inclination: | 43.0043° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 96.1819° |
| argument of perigee: | 270.0919° |
| revolutions per day: | 15.27564770 |
| mean anomaly at epoch: | 89.9758° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|