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 26549U 00057E 24256.84470962 .00007449 00000-0 82024-3 0 9990
2 26549 64.5502 203.9505 0035955 215.7578 144.1123 14.87736615295916
| Epoch (UTC): | 12 September 2024 20:16:22 |
| Eccentricity: | 0.0035955 |
| inclination: | 64.5502° |
| perigee height: | 580 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 203.9505° |
| argument of perigee: | 215.7578° |
| revolutions per day: | 14.87736615 |
| mean anomaly at epoch: | 144.1123° |
| orbit number at epoch: | 29591 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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