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 14506U 83113A 23151.91822392 .00000290 00000-0 13223-3 0 9995
2 14506 98.2978 327.2754 0009823 278.2781 209.6040 14.28515143 56611
Epoch (UTC): | 31 May 2023 22:02:14 |
Eccentricity: | 0.0009823 |
inclination: | 98.2978° |
perigee height: | 789 km |
apogee height: | 804 km |
right ascension of ascending node: | 327.2754° |
argument of perigee: | 278.2781° |
revolutions per day: | 14.28515143 |
mean anomaly at epoch: | 209.6040° |
orbit number at epoch: | 5661 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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