View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 05104U 71024A 25133.77282921 .00000038 00000-0 13843-3 0 9999
2 05104 88.1732 20.0141 0044608 27.6858 37.7494 12.67877970504138
Epoch (UTC): | 13 May 2025 18:32:52 |
Eccentricity: | 0.0044608 |
inclination: | 88.1732° |
perigee height: | 1356 km |
apogee height: | 1425 km |
right ascension of ascending node: | 20.0141° |
argument of perigee: | 27.6858° |
revolutions per day: | 12.67877970 |
mean anomaly at epoch: | 37.7494° |
orbit number at epoch: | 50413 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|