View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58215U 26145.33231492 +.00000000 +00000-0 +47018-4 0 00003
2 58215 43.0026 121.1553 0001393 268.8930 91.1762 15.27580527 06
| Epoch (UTC): | 25 May 2026 07:58:32 |
| Eccentricity: | 0.0001393 |
| inclination: | 43.0026° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 121.1553° |
| argument of perigee: | 268.8930° |
| revolutions per day: | 15.27580527 |
| mean anomaly at epoch: | 91.1762° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|