View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00082U 61004B 24311.89597380 .00001834 00000-0 15246-2 0 9997
2 00082 38.8654 20.3381 1166844 264.0530 82.6263 12.27210832 4620
Epoch (UTC): | 06 November 2024 21:30:12 |
Eccentricity: | 0.1166844 |
inclination: | 38.8654° |
perigee height: | 635 km |
apogee height: | 2487 km |
right ascension of ascending node: | 20.3381° |
argument of perigee: | 264.0530° |
revolutions per day: | 12.27210832 |
mean anomaly at epoch: | 82.6263° |
orbit number at epoch: | 462 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|