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 12:13:00 |
| Eccentricity: | 0.0045337 |
| inclination: | 97.7634° |
| perigee height: | 575 km |
| apogee height: | 639 km |
| right ascension of ascending node: | 169.2544° |
| argument of perigee: | 217.1722° |
| revolutions per day: | 14.87091404 |
| mean anomaly at epoch: | 142.6353° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|