View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
| Epoch (UTC): | 16 January 2026 07:24:40 |
| Eccentricity: | 0.0005113 |
| inclination: | 97.7700° |
| perigee height: | 518 km |
| apogee height: | 525 km |
| right ascension of ascending node: | 30.5128° |
| argument of perigee: | 256.9223° |
| revolutions per day: | 15.14949698 |
| mean anomaly at epoch: | 103.1438° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|