View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 22825U 93061C 24311.45039618 .00000732 00000-0 29758-3 0 9991
2 22825 98.7703 5.5908 0008846 29.7067 330.4616 14.30645692622956
Epoch (UTC): | 06 November 2024 10:48:34 |
Eccentricity: | 0.0008846 |
inclination: | 98.7703° |
perigee height: | 783 km |
apogee height: | 796 km |
right ascension of ascending node: | 5.5908° |
argument of perigee: | 29.7067° |
revolutions per day: | 14.30645692 |
mean anomaly at epoch: | 330.4616° |
orbit number at epoch: | 62295 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|