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 06:45:07 |
| Eccentricity: | 0.0025550 |
| inclination: | 81.1463° |
| perigee height: | 476 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 259.6515° |
| argument of perigee: | 359.8091° |
| revolutions per day: | 15.24013254 |
| mean anomaly at epoch: | 0.3127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|