View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
| Epoch (UTC): | 14 January 2026 12:08:50 |
| Eccentricity: | 0.0885757 |
| inclination: | 63.2942° |
| perigee height: | 380 km |
| apogee height: | 1694 km |
| right ascension of ascending node: | 196.9391° |
| argument of perigee: | 70.2547° |
| revolutions per day: | 13.59633182 |
| mean anomaly at epoch: | 299.1762° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|