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 24309.50428418 .00002836 00000-0 16376-2 0 9992
2 00012 32.9039 141.5360 1652418 225.1320 120.2778 11.47356371463540
Epoch (UTC): | 04 November 2024 12:06:10 |
Eccentricity: | 0.1652418 |
inclination: | 32.9039° |
perigee height: | 553 km |
apogee height: | 3297 km |
right ascension of ascending node: | 141.5360° |
argument of perigee: | 225.1320° |
revolutions per day: | 11.47356371 |
mean anomaly at epoch: | 120.2778° |
orbit number at epoch: | 46354 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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