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 02:21:05 |
| Eccentricity: | 0.0061140 |
| inclination: | 81.2932° |
| perigee height: | 823 km |
| apogee height: | 911 km |
| right ascension of ascending node: | 277.3957° |
| argument of perigee: | 87.7790° |
| revolutions per day: | 14.07733995 |
| mean anomaly at epoch: | 273.0378° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|