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 43760U 18099C 23155.16386300 .00010700 00000-0 73536-3 0 9995
2 43760 97.5676 221.3009 0010524 141.5956 218.6022 15.06073297245891
Epoch (UTC): | 04 June 2023 03:55:57 |
Eccentricity: | 0.0010524 |
inclination: | 97.5676° |
perigee height: | 541 km |
apogee height: | 555 km |
right ascension of ascending node: | 221.3009° |
argument of perigee: | 141.5956° |
revolutions per day: | 15.06073297 |
mean anomaly at epoch: | 218.6022° |
orbit number at epoch: | 24589 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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