View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
| Epoch (UTC): | 12 January 2026 07:55:35 |
| Eccentricity: | 0.0019663 |
| inclination: | 74.0221° |
| perigee height: | 952 km |
| apogee height: | 981 km |
| right ascension of ascending node: | 81.1642° |
| argument of perigee: | 80.0492° |
| revolutions per day: | 13.79145045 |
| mean anomaly at epoch: | 350.8427° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|