View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59184U 26145.37578095 +.00000000 +00000-0 +60745-4 0 00008
2 59184 43.0065 19.1122 0001319 286.1979 73.8727 15.27578653 02
| Epoch (UTC): | 25 May 2026 09:01:07 |
| Eccentricity: | 0.0001319 |
| inclination: | 43.0065° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 19.1122° |
| argument of perigee: | 286.1979° |
| revolutions per day: | 15.27578653 |
| mean anomaly at epoch: | 73.8727° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|