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 43258U 18030K 24357.93471139 -.00000187 00000-0 -73912-4 0 9996
2 43258 86.3995 156.7967 0001481 106.4557 253.6802 14.34218153352544
Epoch (UTC): | 22 December 2024 22:25:59 |
Eccentricity: | 0.0001481 |
inclination: | 86.3995° |
perigee height: | 776 km |
apogee height: | 779 km |
right ascension of ascending node: | 156.7967° |
argument of perigee: | 106.4557° |
revolutions per day: | 14.34218153 |
mean anomaly at epoch: | 253.6802° |
orbit number at epoch: | 35254 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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