View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
| Epoch (UTC): | 14 January 2026 22:15:31 |
| Eccentricity: | 0.0063451 |
| inclination: | 61.9946° |
| perigee height: | 522 km |
| apogee height: | 610 km |
| right ascension of ascending node: | 44.0109° |
| argument of perigee: | 100.3937° |
| revolutions per day: | 15.00240411 |
| mean anomaly at epoch: | 260.4313° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|