View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 16682U 86030B 24311.25796855 .00001467 00000-0 50434-3 0 9995
2 16682 74.0241 307.9140 0014903 346.2099 24.4440 14.36859295 18624
Epoch (UTC): | 06 November 2024 06:11:28 |
Eccentricity: | 0.0014903 |
inclination: | 74.0241° |
perigee height: | 758 km |
apogee height: | 779 km |
right ascension of ascending node: | 307.9140° |
argument of perigee: | 346.2099° |
revolutions per day: | 14.36859295 |
mean anomaly at epoch: | 24.4440° |
orbit number at epoch: | 1862 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|