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 15755U 85042A 23151.30678013 -.00000008 00000-0 18151-4 0 9991
2 15755 71.1112 102.3501 0037543 273.6651 86.0182 14.20580914969151
| Epoch (UTC): | 31 May 2023 07:21:45 |
| Eccentricity: | 0.0037543 |
| inclination: | 71.1112° |
| perigee height: | 796 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 102.3501° |
| argument of perigee: | 273.6651° |
| revolutions per day: | 14.20580914 |
| mean anomaly at epoch: | 86.0182° |
| orbit number at epoch: | 96915 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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