View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 22566U 93016B 24310.60649822 .00000078 00000-0 64568-4 0 9995
2 22566 71.0072 162.3243 0011224 335.6541 24.4050 14.15192189632971
Epoch (UTC): | 05 November 2024 14:33:21 |
Eccentricity: | 0.0011224 |
inclination: | 71.0072° |
perigee height: | 833 km |
apogee height: | 850 km |
right ascension of ascending node: | 162.3243° |
argument of perigee: | 335.6541° |
revolutions per day: | 14.15192189 |
mean anomaly at epoch: | 24.4050° |
orbit number at epoch: | 63297 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|