View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00050U 60009B 25189.21955452 -.00000105 00000-0 -17673-3 0 9993
2 00050 47.2286 149.3799 0112922 69.4316 291.8547 12.20156568895705
Epoch (UTC): | 08 July 2025 05:16:09 |
Eccentricity: | 0.0112922 |
inclination: | 47.2286° |
perigee height: | 1502 km |
apogee height: | 1682 km |
right ascension of ascending node: | 149.3799° |
argument of perigee: | 69.4316° |
revolutions per day: | 12.20156568 |
mean anomaly at epoch: | 291.8547° |
orbit number at epoch: | 89570 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|