View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 50U 60009B 24313.36491823 -.00000021 00000-0 62258-3 0 9999
2 50 47.2286 180.0707 0113827 68.7497 292.5405 12.20149445866630
Epoch (UTC): | 08 November 2024 08:45:28 |
Eccentricity: | 0.0113827 |
inclination: | 47.2286° |
perigee height: | 1501 km |
apogee height: | 1682 km |
right ascension of ascending node: | 180.0707° |
argument of perigee: | 68.7497° |
revolutions per day: | 12.20149445 |
mean anomaly at epoch: | 292.5405° |
orbit number at epoch: | 86663 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|