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 10:19:33 |
| Eccentricity: | 0.0017200 |
| inclination: | 74.0009° |
| perigee height: | 751 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 353.7854° |
| argument of perigee: | 138.5651° |
| revolutions per day: | 14.38578887 |
| mean anomaly at epoch: | 339.0181° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|