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 23153.20798748 -.00000086 00000-0 -17632-4 0 9990
2 15755 71.1114 98.3435 0037506 270.8556 88.8273 14.20581140969697
| Epoch (UTC): | 02 June 2023 04:59:30 |
| Eccentricity: | 0.0037506 |
| inclination: | 71.1114° |
| perigee height: | 796 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 98.3435° |
| argument of perigee: | 270.8556° |
| revolutions per day: | 14.20581140 |
| mean anomaly at epoch: | 88.8273° |
| orbit number at epoch: | 96969 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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