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 23146.84183789 .00004887 00000-0 62361-3 0 9998
2 29110 98.4339 331.1134 0004324 67.7267 57.7898 14.81957757916245
| Epoch (UTC): | 26 May 2023 20:12:14 |
| Eccentricity: | 0.0004324 |
| inclination: | 98.4339° |
| perigee height: | 620 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 331.1134° |
| argument of perigee: | 67.7267° |
| revolutions per day: | 14.81957757 |
| mean anomaly at epoch: | 57.7898° |
| orbit number at epoch: | 91624 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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