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 14:45:19 |
| Eccentricity: | 0.0006702 |
| inclination: | 98.1099° |
| perigee height: | 563 km |
| apogee height: | 573 km |
| right ascension of ascending node: | 203.3783° |
| argument of perigee: | 312.4848° |
| revolutions per day: | 14.99663030 |
| mean anomaly at epoch: | 47.5807° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|