View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00107U 61013A 24262.52967569 .00004909 00000-0 60755-3 0 9992
2 00107 28.7905 14.2773 0515773 323.5351 33.1124 14.16692784185933
Epoch (UTC): | 18 September 2024 12:42:43 |
Eccentricity: | 0.0515773 |
inclination: | 28.7905° |
perigee height: | 464 km |
apogee height: | 1208 km |
right ascension of ascending node: | 14.2773° |
argument of perigee: | 323.5351° |
revolutions per day: | 14.16692784 |
mean anomaly at epoch: | 33.1124° |
orbit number at epoch: | 18593 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|