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 18:44:00 |
| Eccentricity: | 0.0030039 |
| inclination: | 82.9478° |
| perigee height: | 948 km |
| apogee height: | 992 km |
| right ascension of ascending node: | 118.1774° |
| argument of perigee: | 75.4560° |
| revolutions per day: | 13.78285402 |
| mean anomaly at epoch: | 39.4769° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|