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 24280.46866349 .00002039 00000-0 71134-3 0 9999
2 39090 98.3813 105.7196 0007797 282.4271 77.6042 14.36330155608214
| Epoch (UTC): | 06 October 2024 11:14:52 |
| Eccentricity: | 0.0007797 |
| inclination: | 98.3813° |
| perigee height: | 765 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 105.7196° |
| argument of perigee: | 282.4271° |
| revolutions per day: | 14.36330155 |
| mean anomaly at epoch: | 77.6042° |
| orbit number at epoch: | 60821 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|