View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52791U 26145.56016140 +.00000000 +00000-0 +21650-3 0 00005
2 52791 49.9896 306.0004 0012433 9.3681 350.7486 14.81300529 00
| Epoch (UTC): | 25 May 2026 13:26:37 |
| Eccentricity: | 0.0012433 |
| inclination: | 49.9896° |
| perigee height: | 617 km |
| apogee height: | 634 km |
| right ascension of ascending node: | 306.0004° |
| argument of perigee: | 9.3681° |
| revolutions per day: | 14.81300529 |
| mean anomaly at epoch: | 350.7486° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|