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 17590U 87027B 24284.40640876 .00000391 00000-0 21836-3 0 9997
2 17590 71.0012 282.2170 0005858 211.1927 148.8850 14.17025640942386
| Epoch (UTC): | 10 October 2024 09:45:13 |
| Eccentricity: | 0.0005858 |
| inclination: | 71.0012° |
| perigee height: | 831 km |
| apogee height: | 839 km |
| right ascension of ascending node: | 282.2170° |
| argument of perigee: | 211.1927° |
| revolutions per day: | 14.17025640 |
| mean anomaly at epoch: | 148.8850° |
| orbit number at epoch: | 94238 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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