View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
| Epoch (UTC): | 14 January 2026 14:51:35 |
| Eccentricity: | 0.0001705 |
| inclination: | 98.7680° |
| perigee height: | 793 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 332.7563° |
| argument of perigee: | 118.3340° |
| revolutions per day: | 14.29234800 |
| mean anomaly at epoch: | 241.8014° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|