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 19687U 88109A 23334.18369045 .00000066 00000-0 00000+0 0 9999
2 19687 13.9838 343.7244 0005908 249.3018 292.4894 0.99672364108958
Epoch (UTC): | 30 November 2023 04:24:30 |
Eccentricity: | 0.0005908 |
inclination: | 13.9838° |
perigee height: | 35930 km |
apogee height: | 35980 km |
right ascension of ascending node: | 343.7244° |
argument of perigee: | 249.3018° |
revolutions per day: | 0.99672364 |
mean anomaly at epoch: | 292.4894° |
orbit number at epoch: | 10895 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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