View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00116U 26131.83746485 +.00000000 +00000-0 +40146-4 0 00008
2 00116 66.8103 339.7787 0081507 296.3147 62.9577 13.92325682 08
| Epoch (UTC): | 11 May 2026 20:05:56 |
| Eccentricity: | 0.0081507 |
| inclination: | 66.8103° |
| perigee height: | 861 km |
| apogee height: | 980 km |
| right ascension of ascending node: | 339.7787° |
| argument of perigee: | 296.3147° |
| revolutions per day: | 13.92325682 |
| mean anomaly at epoch: | 62.9577° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|