View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58116U 26145.46376713 +.00000000 +00000-0 -43589-4 0 00003
2 58116 53.1594 169.0961 0001165 80.9465 279.1668 15.30183857 07
| Epoch (UTC): | 25 May 2026 11:07:49 |
| Eccentricity: | 0.0001165 |
| inclination: | 53.1594° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 169.0961° |
| argument of perigee: | 80.9465° |
| revolutions per day: | 15.30183857 |
| mean anomaly at epoch: | 279.1668° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|