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 33504U 09003A 25193.87923312 .00005267 00000-0 14381-3 0 9992
2 33504 82.4330 163.8947 0009866 302.0898 57.9388 15.37120721908831
Epoch (UTC): | 12 July 2025 21:06:05 |
Eccentricity: | 0.0009866 |
inclination: | 82.4330° |
perigee height: | 448 km |
apogee height: | 461 km |
right ascension of ascending node: | 163.8947° |
argument of perigee: | 302.0898° |
revolutions per day: | 15.37120721 |
mean anomaly at epoch: | 57.9388° |
orbit number at epoch: | 90883 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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