View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 33591U 09005A 24286.83992412 .00000807 00000-0 45568-3 0 9991
2 33591 99.0338 343.8151 0013082 323.7555 36.2729 14.13155217807985
Epoch (UTC): | 12 October 2024 20:09:29 |
Eccentricity: | 0.0013082 |
inclination: | 99.0338° |
perigee height: | 839 km |
apogee height: | 858 km |
right ascension of ascending node: | 343.8151° |
argument of perigee: | 323.7555° |
revolutions per day: | 14.13155217 |
mean anomaly at epoch: | 36.2729° |
orbit number at epoch: | 80798 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|