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 14148U 83061B 23028.05606997 .00000741 00000-0 86397-4 0 9992
2 14148 82.5211 148.3981 0022571 54.2934 306.0376 14.83699615138860
Epoch (UTC): | 28 January 2023 01:20:44 |
Eccentricity: | 0.0022571 |
inclination: | 82.5211° |
perigee height: | 602 km |
apogee height: | 633 km |
right ascension of ascending node: | 148.3981° |
argument of perigee: | 54.2934° |
revolutions per day: | 14.83699615 |
mean anomaly at epoch: | 306.0376° |
orbit number at epoch: | 13886 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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