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 03093U 68002A 23337.62903260 -.00000080 00000-0 -14763-4 0 9992
2 03093 105.7988 201.6987 0318770 169.8972 205.2306 12.83566688618473
Epoch (UTC): | 03 December 2023 15:05:48 |
Eccentricity: | 0.0318770 |
inclination: | 105.7988° |
perigee height: | 1081 km |
apogee height: | 1573 km |
right ascension of ascending node: | 201.6987° |
argument of perigee: | 169.8972° |
revolutions per day: | 12.83566688 |
mean anomaly at epoch: | 205.2306° |
orbit number at epoch: | 61847 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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