View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 28485U 04047A 24311.48275487 .00040717 00000-0 15045-2 0 9994
2 28485 20.5554 238.0309 0007474 322.3680 37.6234 15.25996422 95881
Epoch (UTC): | 06 November 2024 11:35:10 |
Eccentricity: | 0.0007474 |
inclination: | 20.5554° |
perigee height: | 482 km |
apogee height: | 493 km |
right ascension of ascending node: | 238.0309° |
argument of perigee: | 322.3680° |
revolutions per day: | 15.25996422 |
mean anomaly at epoch: | 37.6234° |
orbit number at epoch: | 9588 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|