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 13121U 82027B 25191.65056705 .00003468 00000-0 13955-3 0 9996
2 13121 81.1906 322.9129 0009437 22.2545 337.9095 15.24581194361631
Epoch (UTC): | 10 July 2025 15:36:48 |
Eccentricity: | 0.0009437 |
inclination: | 81.1906° |
perigee height: | 485 km |
apogee height: | 498 km |
right ascension of ascending node: | 322.9129° |
argument of perigee: | 22.2545° |
revolutions per day: | 15.24581194 |
mean anomaly at epoch: | 337.9095° |
orbit number at epoch: | 36163 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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