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 17153U 86019AG 24357.99315176 .00006735 00000-0 13369-2 0 9998
2 17153 98.0027 5.1559 0014467 178.0522 182.0738 14.62426676956022
| Epoch (UTC): | 22 December 2024 23:50:08 |
| Eccentricity: | 0.0014467 |
| inclination: | 98.0027° |
| perigee height: | 675 km |
| apogee height: | 695 km |
| right ascension of ascending node: | 5.1559° |
| argument of perigee: | 178.0522° |
| revolutions per day: | 14.62426676 |
| mean anomaly at epoch: | 182.0738° |
| orbit number at epoch: | 95602 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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