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 19257U 88053B 24284.55018713 .00001279 00000-0 42700-3 0 9993
2 19257 74.0493 341.6499 0021467 289.6608 176.1569 14.38386467902510
| Epoch (UTC): | 10 October 2024 13:12:16 |
| Eccentricity: | 0.0021467 |
| inclination: | 74.0493° |
| perigee height: | 748 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 341.6499° |
| argument of perigee: | 289.6608° |
| revolutions per day: | 14.38386467 |
| mean anomaly at epoch: | 176.1569° |
| orbit number at epoch: | 90251 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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