View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00022U 59009A 25191.58922527 .00006514 00000-0 28490-3 0 9997
2 00022 50.2736 337.1716 0091162 196.8688 162.9232 15.19596815748242
| Epoch (UTC): | 10 July 2025 14:08:29 |
| Eccentricity: | 0.0091162 |
| inclination: | 50.2736° |
| perigee height: | 444 km |
| apogee height: | 570 km |
| right ascension of ascending node: | 337.1716° |
| argument of perigee: | 196.8688° |
| revolutions per day: | 15.19596815 |
| mean anomaly at epoch: | 162.9232° |
| orbit number at epoch: | 74824 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|