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 25138.19272775 .00000730 00000-0 41769-3 0 9997
2 12 32.8961 176.5347 1649316 174.4128 187.7575 11.47727070728490
Epoch (UTC): | 18 May 2025 04:37:31 |
Eccentricity: | 0.1649316 |
inclination: | 32.8961° |
perigee height: | 554 km |
apogee height: | 3293 km |
right ascension of ascending node: | 176.5347° |
argument of perigee: | 174.4128° |
revolutions per day: | 11.47727070 |
mean anomaly at epoch: | 187.7575° |
orbit number at epoch: | 72849 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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