View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39430U 26073.93299681 +.00000000 +00000-0 +35296-3 0 00005
2 39430 97.6571 280.3111 0129920 20.7697 339.8721 14.69120759 03
| Epoch (UTC): | 14 March 2026 22:23:30 |
| Eccentricity: | 0.0129920 |
| inclination: | 97.6571° |
| perigee height: | 572 km |
| apogee height: | 755 km |
| right ascension of ascending node: | 280.3111° |
| argument of perigee: | 20.7697° |
| revolutions per day: | 14.69120759 |
| mean anomaly at epoch: | 339.8721° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|