View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 13403U 82079B 25194.59557298 .00003976 00000-0 17396-3 0 9992
2 13403 81.1485 114.6869 0024706 252.8213 107.0313 15.21550012341305
Epoch (UTC): | 13 July 2025 14:17:37 |
Eccentricity: | 0.0024706 |
inclination: | 81.1485° |
perigee height: | 484 km |
apogee height: | 518 km |
right ascension of ascending node: | 114.6869° |
argument of perigee: | 252.8213° |
revolutions per day: | 15.21550012 |
mean anomaly at epoch: | 107.0313° |
orbit number at epoch: | 34130 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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