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 18:58:10 |
| Eccentricity: | 0.4948918 |
| inclination: | 49.4513° |
| perigee height: | 276 km |
| apogee height: | 13314 km |
| right ascension of ascending node: | 216.0842° |
| argument of perigee: | 84.1500° |
| revolutions per day: | 5.74236336 |
| mean anomaly at epoch: | 328.0190° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|