View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
| Epoch (UTC): | 13 January 2026 13:02:26 |
| Eccentricity: | 0.0036479 |
| inclination: | 71.1063° |
| perigee height: | 792 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 204.2320° |
| argument of perigee: | 214.4184° |
| revolutions per day: | 14.21962002 |
| mean anomaly at epoch: | 209.7714° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|