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 24317.77242963 .00001960 00000-0 11224-2 0 9993
2 00012 32.9088 112.4612 1652708 268.8095 72.3511 11.47395588464496
Epoch (UTC): | 12 November 2024 18:32:17 |
Eccentricity: | 0.1652708 |
inclination: | 32.9088° |
perigee height: | 553 km |
apogee height: | 3297 km |
right ascension of ascending node: | 112.4612° |
argument of perigee: | 268.8095° |
revolutions per day: | 11.47395588 |
mean anomaly at epoch: | 72.3511° |
orbit number at epoch: | 46449 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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