View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
| Epoch (UTC): | 15 January 2026 03:05:54 |
| Eccentricity: | 0.0018972 |
| inclination: | 70.7594° |
| perigee height: | 837 km |
| apogee height: | 865 km |
| right ascension of ascending node: | 288.6095° |
| argument of perigee: | 220.2121° |
| revolutions per day: | 14.12400829 |
| mean anomaly at epoch: | 139.7596° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|