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 16:19:36 |
| Eccentricity: | 0.0001493 |
| inclination: | 97.7590° |
| perigee height: | 605 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 40.1051° |
| argument of perigee: | 86.3580° |
| revolutions per day: | 14.87449576 |
| mean anomaly at epoch: | 273.7807° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|