View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 39090U 13009E 24260.96286379 .00001256 00000-0 44422-3 0 9991
2 39090 98.3820 86.7400 0008545 346.1103 13.9848 14.36277471605419
| Epoch (UTC): | 16 September 2024 23:06:31 |
| Eccentricity: | 0.0008545 |
| inclination: | 98.3820° |
| perigee height: | 765 km |
| apogee height: | 777 km |
| right ascension of ascending node: | 86.7400° |
| argument of perigee: | 346.1103° |
| revolutions per day: | 14.36277471 |
| mean anomaly at epoch: | 13.9848° |
| orbit number at epoch: | 60541 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|