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 29110U 06016D 23151.56188750 .00005970 00000-0 75915-3 0 9999
2 29110 98.4331 336.0838 0004155 55.6955 36.7962 14.82010606916944
| Epoch (UTC): | 31 May 2023 13:29:07 |
| Eccentricity: | 0.0004155 |
| inclination: | 98.4331° |
| perigee height: | 620 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 336.0838° |
| argument of perigee: | 55.6955° |
| revolutions per day: | 14.82010606 |
| mean anomaly at epoch: | 36.7962° |
| orbit number at epoch: | 91694 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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