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 02:31:22 |
| Eccentricity: | 0.0869036 |
| inclination: | 82.4878° |
| perigee height: | 399 km |
| apogee height: | 1688 km |
| right ascension of ascending node: | 273.8589° |
| argument of perigee: | 241.7242° |
| revolutions per day: | 13.57852141 |
| mean anomaly at epoch: | 109.3587° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|