View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 11086U 26065.45037424 +.00000000 +00000-0 -32846-3 0 00004
2 11086 82.5444 102.4645 0012817 168.8915 256.8426 11.96753000 09
| Epoch (UTC): | 06 March 2026 10:48:32 |
| Eccentricity: | 0.0012817 |
| inclination: | 82.5444° |
| perigee height: | 1685 km |
| apogee height: | 1706 km |
| right ascension of ascending node: | 102.4645° |
| argument of perigee: | 168.8915° |
| revolutions per day: | 11.96753000 |
| mean anomaly at epoch: | 256.8426° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|