View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 51650U 26145.58155845 +.00000000 +00000-0 -11953-4 0 00003
2 51650 87.9151 10.3755 0001795 89.2926 270.8411 13.17649459 01
| Epoch (UTC): | 25 May 2026 13:57:26 |
| Eccentricity: | 0.0001795 |
| inclination: | 87.9151° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.3755° |
| argument of perigee: | 89.2926° |
| revolutions per day: | 13.17649459 |
| mean anomaly at epoch: | 270.8411° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|