View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 60713U 24140DS 24357.85009352 .00000394 00000-0 18063-3 0 9998
2 60713 89.0265 336.0122 0050258 120.4209 240.1961 14.18729684 18837
| Epoch (UTC): | 22 December 2024 20:24:08 |
| Eccentricity: | 0.0050258 |
| inclination: | 89.0265° |
| perigee height: | 793 km |
| apogee height: | 866 km |
| right ascension of ascending node: | 336.0122° |
| argument of perigee: | 120.4209° |
| revolutions per day: | 14.18729684 |
| mean anomaly at epoch: | 240.1961° |
| orbit number at epoch: | 1883 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|