View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
| Epoch (UTC): | 13 January 2026 06:16:04 |
| Eccentricity: | 0.0063475 |
| inclination: | 61.9947° |
| perigee height: | 522 km |
| apogee height: | 610 km |
| right ascension of ascending node: | 49.7990° |
| argument of perigee: | 99.9752° |
| revolutions per day: | 15.00237046 |
| mean anomaly at epoch: | 260.8509° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|