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 05:00:55 |
| Eccentricity: | 0.0007741 |
| inclination: | 51.6330° |
| perigee height: | 414 km |
| apogee height: | 424 km |
| right ascension of ascending node: | 346.6801° |
| argument of perigee: | 12.6584° |
| revolutions per day: | 15.49269250 |
| mean anomaly at epoch: | 347.4598° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|