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 30341U 99025ABC 24358.05909220 .00014607 00000-0 58658-2 0 9997
2 30341 99.2252 218.4602 0057273 5.0220 136.9729 14.27363476920447
Epoch (UTC): | 23 December 2024 01:25:05 |
Eccentricity: | 0.0057273 |
inclination: | 99.2252° |
perigee height: | 759 km |
apogee height: | 841 km |
right ascension of ascending node: | 218.4602° |
argument of perigee: | 5.0220° |
revolutions per day: | 14.27363476 |
mean anomaly at epoch: | 136.9729° |
orbit number at epoch: | 92044 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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