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 14:57:18 |
| Eccentricity: | 0.0030654 |
| inclination: | 82.9335° |
| perigee height: | 948 km |
| apogee height: | 993 km |
| right ascension of ascending node: | 123.9599° |
| argument of perigee: | 171.3198° |
| revolutions per day: | 13.78257922 |
| mean anomaly at epoch: | 188.8497° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|