View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00047U 60007C 24315.90654563 .00002277 00000-0 50963-3 0 9991
2 00047 66.6647 173.0303 0225872 207.9430 150.9399 14.44089413366544
Epoch (UTC): | 10 November 2024 21:45:25 |
Eccentricity: | 0.0225872 |
inclination: | 66.6647° |
perigee height: | 584 km |
apogee height: | 906 km |
right ascension of ascending node: | 173.0303° |
argument of perigee: | 207.9430° |
revolutions per day: | 14.44089413 |
mean anomaly at epoch: | 150.9399° |
orbit number at epoch: | 36654 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|