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 24313.50749045 .00002441 00000-0 14036-2 0 9992
2 12 32.9070 127.4584 1652553 246.2794 95.6139 11.47376668706586
Epoch (UTC): | 08 November 2024 12:10:47 |
Eccentricity: | 0.1652553 |
inclination: | 32.9070° |
perigee height: | 553 km |
apogee height: | 3297 km |
right ascension of ascending node: | 127.4584° |
argument of perigee: | 246.2794° |
revolutions per day: | 11.47376668 |
mean anomaly at epoch: | 95.6139° |
orbit number at epoch: | 70658 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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