View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 59588U 24077B 25165.27907695 .00007616 00000-0 74526-2 0 9995
2 59588 97.4742 160.2333 0063812 81.9982 278.8410 13.78349492 57096
| Epoch (UTC): | 14 June 2025 06:41:52 |
| Eccentricity: | 0.0063812 |
| inclination: | 97.4742° |
| perigee height: | 923 km |
| apogee height: | 1016 km |
| right ascension of ascending node: | 160.2333° |
| argument of perigee: | 81.9982° |
| revolutions per day: | 13.78349492 |
| mean anomaly at epoch: | 278.8410° |
| orbit number at epoch: | 5709 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|