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 00012U 59001B 24311.85392084 .00002526 00000-0 14549-2 0 9998
2 00012 32.9055 133.2732 1652448 237.5442 105.4709 11.47368524463816
Epoch (UTC): | 06 November 2024 20:29:38 |
Eccentricity: | 0.1652448 |
inclination: | 32.9055° |
perigee height: | 553 km |
apogee height: | 3297 km |
right ascension of ascending node: | 133.2732° |
argument of perigee: | 237.5442° |
revolutions per day: | 11.47368524 |
mean anomaly at epoch: | 105.4709° |
orbit number at epoch: | 46381 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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