View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
| Epoch (UTC): | 15 January 2026 01:27:53 |
| Eccentricity: | 0.0021624 |
| inclination: | 74.0395° |
| perigee height: | 750 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 227.0126° |
| argument of perigee: | 345.7330° |
| revolutions per day: | 14.37921278 |
| mean anomaly at epoch: | 14.3210° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|