View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00053U 60009E 24316.16549958 -.00000062 00000-0 22910-3 0 9992
2 00053 47.2785 340.7263 0098444 153.7803 206.8015 12.17355160864409
Epoch (UTC): | 11 November 2024 03:58:19 |
Eccentricity: | 0.0098444 |
inclination: | 47.2785° |
perigee height: | 1525 km |
apogee height: | 1682 km |
right ascension of ascending node: | 340.7263° |
argument of perigee: | 153.7803° |
revolutions per day: | 12.17355160 |
mean anomaly at epoch: | 206.8015° |
orbit number at epoch: | 86440 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|