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 03:23:35 |
| Eccentricity: | 0.0018413 |
| inclination: | 82.4929° |
| perigee height: | 611 km |
| apogee height: | 637 km |
| right ascension of ascending node: | 270.4055° |
| argument of perigee: | 59.6017° |
| revolutions per day: | 14.81774003 |
| mean anomaly at epoch: | 300.7014° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|