View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 37224U 10062C 24280.74637847 .00011485 00000-0 12328-2 0 9996
2 37224 71.9747 36.6609 0014743 169.9849 190.1616 14.88636630 24421
Epoch (UTC): | 06 October 2024 17:54:47 |
Eccentricity: | 0.0014743 |
inclination: | 71.9747° |
perigee height: | 592 km |
apogee height: | 612 km |
right ascension of ascending node: | 36.6609° |
argument of perigee: | 169.9849° |
revolutions per day: | 14.88636630 |
mean anomaly at epoch: | 190.1616° |
orbit number at epoch: | 2442 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|