View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 20508U 90017A 25133.78539843 .00000071 00000-0 58510-4 0 9994
2 20508 82.9584 9.0856 0045306 112.6069 317.8239 13.74508835765515
Epoch (UTC): | 13 May 2025 18:50:58 |
Eccentricity: | 0.0045306 |
inclination: | 82.9584° |
perigee height: | 950 km |
apogee height: | 1017 km |
right ascension of ascending node: | 9.0856° |
argument of perigee: | 112.6069° |
revolutions per day: | 13.74508835 |
mean anomaly at epoch: | 317.8239° |
orbit number at epoch: | 76551 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|