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 23150.32096896 .00000049 00000-0 44507-4 0 9993
2 15755 71.1110 104.4276 0037539 275.1139 84.5703 14.20580739969016
| Epoch (UTC): | 30 May 2023 07:42:11 |
| Eccentricity: | 0.0037539 |
| inclination: | 71.1110° |
| perigee height: | 796 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 104.4276° |
| argument of perigee: | 275.1139° |
| revolutions per day: | 14.20580739 |
| mean anomaly at epoch: | 84.5703° |
| orbit number at epoch: | 96901 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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