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 11511U 79078B 24276.96566607 .00001460 00000-0 49307-3 0 9993
2 11511 74.0337 95.4403 0014737 46.2682 313.9689 14.37750480361390
| Epoch (UTC): | 02 October 2024 23:10:33 |
| Eccentricity: | 0.0014737 |
| inclination: | 74.0337° |
| perigee height: | 755 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 95.4403° |
| argument of perigee: | 46.2682° |
| revolutions per day: | 14.37750480 |
| mean anomaly at epoch: | 313.9689° |
| orbit number at epoch: | 36139 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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