View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 23405U 94077B 24357.89102698 .00000344 00000-0 20085-3 0 9994
2 23405 70.9814 201.8873 0001108 169.8119 190.3026 14.15473901553716
| Epoch (UTC): | 22 December 2024 21:23:04 |
| Eccentricity: | 0.0001108 |
| inclination: | 70.9814° |
| perigee height: | 840 km |
| apogee height: | 841 km |
| right ascension of ascending node: | 201.8873° |
| argument of perigee: | 169.8119° |
| revolutions per day: | 14.15473901 |
| mean anomaly at epoch: | 190.3026° |
| orbit number at epoch: | 55371 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|