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 37841U 11058D 24262.54357905 .00000704 00000-0 23983-3 0 9991
2 37841 19.9725 312.1046 0011901 41.7299 107.6607 14.11210135667767
Epoch (UTC): | 18 September 2024 13:02:45 |
Eccentricity: | 0.0011901 |
inclination: | 19.9725° |
perigee height: | 846 km |
apogee height: | 864 km |
right ascension of ascending node: | 312.1046° |
argument of perigee: | 41.7299° |
revolutions per day: | 14.11210135 |
mean anomaly at epoch: | 107.6607° |
orbit number at epoch: | 66776 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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