View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39089U 26145.49165866 +.00000000 +00000-0 +62451-4 0 00007
2 39089 98.4174 326.0649 0010157 319.2073 40.8352 14.35817339 09
| Epoch (UTC): | 25 May 2026 11:47:59 |
| Eccentricity: | 0.0010157 |
| inclination: | 98.4174° |
| perigee height: | 765 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 326.0649° |
| argument of perigee: | 319.2073° |
| revolutions per day: | 14.35817339 |
| mean anomaly at epoch: | 40.8352° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|