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 26384U 00033A 24260.22664089 .00002928 00000-0 50407-3 0 9990
2 26384 97.7764 251.4131 0012147 236.1902 123.8148 14.69238467295058
| Epoch (UTC): | 16 September 2024 05:26:21 |
| Eccentricity: | 0.0012147 |
| inclination: | 97.7764° |
| perigee height: | 655 km |
| apogee height: | 672 km |
| right ascension of ascending node: | 251.4131° |
| argument of perigee: | 236.1902° |
| revolutions per day: | 14.69238467 |
| mean anomaly at epoch: | 123.8148° |
| orbit number at epoch: | 29505 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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