View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58354U 26145.66425123 +.00000000 +00000-0 +17589-3 0 00008
2 58354 43.0033 276.4013 0001571 271.2094 88.8577 15.27580167 07
| Epoch (UTC): | 25 May 2026 15:56:31 |
| Eccentricity: | 0.0001571 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 276.4013° |
| argument of perigee: | 271.2094° |
| revolutions per day: | 15.27580167 |
| mean anomaly at epoch: | 88.8577° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|