View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 59782C 24093A 25136.42270833 .00015524 00000+0 56238-3 0 1361
2 59782 43.0030 84.4935 0001403 269.0327 278.8378 15.27556675 16
| Epoch (UTC): | 16 May 2025 10:08:42 |
| Eccentricity: | 0.0001403 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 84.4935° |
| argument of perigee: | 269.0327° |
| revolutions per day: | 15.27556675 |
| mean anomaly at epoch: | 278.8378° |
| orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|