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 09:20:08 |
| Eccentricity: | 0.0008195 |
| inclination: | 53.2314° |
| perigee height: | 452 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 39.6750° |
| argument of perigee: | 62.3389° |
| revolutions per day: | 15.36280905 |
| mean anomaly at epoch: | 297.8446° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|