View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 29U 60002B 23332.81653162 .00001836 00000-0 29431-3 0 9994
2 29 48.3774 121.7820 0024067 224.9030 134.9936 14.75760976404528
| Epoch (UTC): | 28 November 2023 19:35:48 |
| Eccentricity: | 0.0024067 |
| inclination: | 48.3774° |
| perigee height: | 626 km |
| apogee height: | 659 km |
| right ascension of ascending node: | 121.7820° |
| argument of perigee: | 224.9030° |
| revolutions per day: | 14.75760976 |
| mean anomaly at epoch: | 134.9936° |
| orbit number at epoch: | 40452 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|