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 17478U 86019HR 24357.54989292 .00001010 00000-0 40425-3 0 9990
2 17478 98.2727 4.7029 0038520 211.1580 278.9811 14.30012542979522
| Epoch (UTC): | 22 December 2024 13:11:50 |
| Eccentricity: | 0.0038520 |
| inclination: | 98.2727° |
| perigee height: | 764 km |
| apogee height: | 819 km |
| right ascension of ascending node: | 4.7029° |
| argument of perigee: | 211.1580° |
| revolutions per day: | 14.30012542 |
| mean anomaly at epoch: | 278.9811° |
| orbit number at epoch: | 97952 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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