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 12U 59001B 25133.23490406 .00000657 00000-0 38137-3 0 9993
2 12 32.8951 193.9864 1649403 148.1826 222.9980 11.47720692727928
Epoch (UTC): | 13 May 2025 05:38:15 |
Eccentricity: | 0.1649403 |
inclination: | 32.8951° |
perigee height: | 554 km |
apogee height: | 3293 km |
right ascension of ascending node: | 193.9864° |
argument of perigee: | 148.1826° |
revolutions per day: | 11.47720692 |
mean anomaly at epoch: | 222.9980° |
orbit number at epoch: | 72792 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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