View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
| Epoch (UTC): | 12 January 2026 06:54:52 |
| Eccentricity: | 0.0002040 |
| inclination: | 28.4671° |
| perigee height: | 479 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 64.4829° |
| argument of perigee: | 194.5967° |
| revolutions per day: | 15.28511891 |
| mean anomaly at epoch: | 165.4569° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|