View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58190U 26145.48225295 +.00000000 +00000-0 +52521-5 0 00001
2 58190 43.0005 69.3576 0001063 247.3783 112.6957 15.27581754 03
| Epoch (UTC): | 25 May 2026 11:34:26 |
| Eccentricity: | 0.0001063 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 69.3576° |
| argument of perigee: | 247.3783° |
| revolutions per day: | 15.27581754 |
| mean anomaly at epoch: | 112.6957° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|