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 14:04:39 |
| Eccentricity: | 0.0024251 |
| inclination: | 97.6112° |
| perigee height: | 439 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 18.2282° |
| argument of perigee: | 62.1432° |
| revolutions per day: | 15.36932098 |
| mean anomaly at epoch: | 298.2264° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|