View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
| Epoch (UTC): | 16 January 2026 05:51:03 |
| Eccentricity: | 0.0013467 |
| inclination: | 70.9996° |
| perigee height: | 833 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 48.0583° |
| argument of perigee: | 14.3348° |
| revolutions per day: | 14.15007840 |
| mean anomaly at epoch: | 345.8154° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|