View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58957U 26145.49575856 +.00000000 +00000-0 +73061-4 0 00005
2 58957 39.9882 148.2079 0011185 123.7307 236.4507 13.70767176 07
| Epoch (UTC): | 25 May 2026 11:53:53 |
| Eccentricity: | 0.0011185 |
| inclination: | 39.9882° |
| perigee height: | 989 km |
| apogee height: | 1005 km |
| right ascension of ascending node: | 148.2079° |
| argument of perigee: | 123.7307° |
| revolutions per day: | 13.70767176 |
| mean anomaly at epoch: | 236.4507° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|