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 24280.95629805 .00002060 00000-0 71867-3 0 9994
2 39090 98.3812 106.1941 0007783 280.7384 79.2926 14.36332195608302
| Epoch (UTC): | 06 October 2024 22:57:04 |
| Eccentricity: | 0.0007783 |
| inclination: | 98.3812° |
| perigee height: | 765 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 106.1941° |
| argument of perigee: | 280.7384° |
| revolutions per day: | 14.36332195 |
| mean anomaly at epoch: | 79.2926° |
| orbit number at epoch: | 60830 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|