View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 07714U 75023A 25188.77320788 .00000045 00000-0 19094-4 0 9998
2 07714 81.1972 205.7164 0028759 240.6458 119.1839 14.08420746899053
| Epoch (UTC): | 07 July 2025 18:33:25 |
| Eccentricity: | 0.0028759 |
| inclination: | 81.1972° |
| perigee height: | 844 km |
| apogee height: | 885 km |
| right ascension of ascending node: | 205.7164° |
| argument of perigee: | 240.6458° |
| revolutions per day: | 14.08420746 |
| mean anomaly at epoch: | 119.1839° |
| orbit number at epoch: | 89905 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|