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 15:13:05 |
| Eccentricity: | 0.0001148 |
| inclination: | 98.3642° |
| perigee height: | 761 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 328.5736° |
| argument of perigee: | 91.4004° |
| revolutions per day: | 14.39012887 |
| mean anomaly at epoch: | 82.0121° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|