View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39440U 26073.32206177 +.00000000 +00000-0 +61815-3 0 00003
2 39440 97.8809 22.0019 0058046 343.6383 16.2961 14.93017334 00
| Epoch (UTC): | 14 March 2026 07:43:46 |
| Eccentricity: | 0.0058046 |
| inclination: | 97.8809° |
| perigee height: | 548 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 22.0019° |
| argument of perigee: | 343.6383° |
| revolutions per day: | 14.93017334 |
| mean anomaly at epoch: | 16.2961° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|