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 29773U 99025BP 24357.40063182 .00002161 00000-0 90603-3 0 9999
2 29773 98.9440 136.0790 0047531 237.1319 187.8233 14.26459554931297
| Epoch (UTC): | 22 December 2024 09:36:54 |
| Eccentricity: | 0.0047531 |
| inclination: | 98.9440° |
| perigee height: | 769 km |
| apogee height: | 838 km |
| right ascension of ascending node: | 136.0790° |
| argument of perigee: | 237.1319° |
| revolutions per day: | 14.26459554 |
| mean anomaly at epoch: | 187.8233° |
| orbit number at epoch: | 93129 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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