View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
| Epoch (UTC): | 17 August 2025 20:16:44 |
| Eccentricity: | 0.4431861 |
| inclination: | 12.6095° |
| perigee height: | 9604 km |
| apogee height: | 35045 km |
| right ascension of ascending node: | 79.7246° |
| argument of perigee: | 224.5089° |
| revolutions per day: | 1.78530791 |
| mean anomaly at epoch: | 89.9343° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|