View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 44682U 26017.33399718 +.00000000 +00000-0 +00000-0 0 00006
2 44682 13.2247 48.9579 4635062 286.4932 28.5972 1.81925038 07
| Epoch (UTC): | 17 January 2026 08:00:57 |
| Eccentricity: | 0.4635062 |
| inclination: | 13.2247° |
| perigee height: | 8829 km |
| apogee height: | 35105 km |
| right ascension of ascending node: | 48.9579° |
| argument of perigee: | 286.4932° |
| revolutions per day: | 1.81925038 |
| mean anomaly at epoch: | 28.5972° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|