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 22:48:15 |
| Eccentricity: | 0.0019303 |
| inclination: | 74.0437° |
| perigee height: | 751 km |
| apogee height: | 778 km |
| right ascension of ascending node: | 217.0788° |
| argument of perigee: | 72.6310° |
| revolutions per day: | 14.38152788 |
| mean anomaly at epoch: | 287.6953° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|