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 61363U 24140WC 24358.38712459 .00004510 00000-0 19430-2 0 9990
2 61363 89.0815 336.7511 0041595 87.0558 273.5393 14.23960272 15784
Epoch (UTC): | 23 December 2024 09:17:27 |
Eccentricity: | 0.0041595 |
inclination: | 89.0815° |
perigee height: | 782 km |
apogee height: | 842 km |
right ascension of ascending node: | 336.7511° |
argument of perigee: | 87.0558° |
revolutions per day: | 14.23960272 |
mean anomaly at epoch: | 273.5393° |
orbit number at epoch: | 1578 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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