View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 22826U 93061D 23265.70210156 .00000228 00000-0 10457-3 0 9991
2 22826 98.8263 309.9838 0009897 125.5694 234.6412 14.30713541564504
Epoch (UTC): | 22 September 2023 16:51:01 |
Eccentricity: | 0.0009897 |
inclination: | 98.8263° |
perigee height: | 782 km |
apogee height: | 796 km |
right ascension of ascending node: | 309.9838° |
argument of perigee: | 125.5694° |
revolutions per day: | 14.30713541 |
mean anomaly at epoch: | 234.6412° |
orbit number at epoch: | 56450 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|