View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 31196U 99025BKA 24284.33360221 .00005437 00000-0 23567-2 0 9999
2 31196 98.5545 303.3101 0059877 24.1358 336.2606 14.23666336573953
Epoch (UTC): | 10 October 2024 08:00:23 |
Eccentricity: | 0.0059877 |
inclination: | 98.5545° |
perigee height: | 770 km |
apogee height: | 856 km |
right ascension of ascending node: | 303.3101° |
argument of perigee: | 24.1358° |
revolutions per day: | 14.23666336 |
mean anomaly at epoch: | 336.2606° |
orbit number at epoch: | 57395 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|