View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 07493U 74083B 24315.47014897 .00000546 00000-0 30469-3 0 9990
2 07493 81.1614 35.6287 0083558 44.1653 316.6146 14.07874779568784
Epoch (UTC): | 10 November 2024 11:17:00 |
Eccentricity: | 0.0083558 |
inclination: | 81.1614° |
perigee height: | 806 km |
apogee height: | 927 km |
right ascension of ascending node: | 35.6287° |
argument of perigee: | 44.1653° |
revolutions per day: | 14.07874779 |
mean anomaly at epoch: | 316.6146° |
orbit number at epoch: | 56878 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|