View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 14781U 84021B 25108.86712902 .00002718 00000-0 29326-3 0 9990
2 14781 97.7504 76.2807 0008868 137.9902 222.1997 14.89180594214947
Epoch (UTC): | 18 April 2025 20:48:39 |
Eccentricity: | 0.0008868 |
inclination: | 97.7504° |
perigee height: | 594 km |
apogee height: | 606 km |
right ascension of ascending node: | 76.2807° |
argument of perigee: | 137.9902° |
revolutions per day: | 14.89180594 |
mean anomaly at epoch: | 222.1997° |
orbit number at epoch: | 21494 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|