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 55326U 23011C 24358.10225805 .00009381 00000-0 49875-3 0 9990
2 55326 40.4840 248.4330 0002297 335.0195 25.0500 15.15197386105535
| Epoch (UTC): | 23 December 2024 02:27:15 |
| Eccentricity: | 0.0002297 |
| inclination: | 40.4840° |
| perigee height: | 519 km |
| apogee height: | 522 km |
| right ascension of ascending node: | 248.4330° |
| argument of perigee: | 335.0195° |
| revolutions per day: | 15.15197386 |
| mean anomaly at epoch: | 25.0500° |
| orbit number at epoch: | 10553 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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