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 15:24:20 |
| Eccentricity: | 0.0007523 |
| inclination: | 97.7171° |
| perigee height: | 626 km |
| apogee height: | 637 km |
| right ascension of ascending node: | 48.5938° |
| argument of perigee: | 43.6995° |
| revolutions per day: | 14.79333494 |
| mean anomaly at epoch: | 79.1455° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|