View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 26931U 01043C 23332.79845526 .00000539 00000-0 23568-3 0 9992
2 26931 67.0496 131.7464 0005848 257.8279 102.2168 14.31053369157138
Epoch (UTC): | 28 November 2023 19:09:46 |
Eccentricity: | 0.0005848 |
inclination: | 67.0496° |
perigee height: | 784 km |
apogee height: | 792 km |
right ascension of ascending node: | 131.7464° |
argument of perigee: | 257.8279° |
revolutions per day: | 14.31053369 |
mean anomaly at epoch: | 102.2168° |
orbit number at epoch: | 15713 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|