View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
| Epoch (UTC): | 16 January 2026 07:45:36 |
| Eccentricity: | 0.0001411 |
| inclination: | 97.5466° |
| perigee height: | 595 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 46.2006° |
| argument of perigee: | 132.2601° |
| revolutions per day: | 14.90538320 |
| mean anomaly at epoch: | 227.8738° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|