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 7175U 73086EM 24357.97254491 .00001176 00000-0 41080-2 0 9996
2 7175 102.5879 127.8146 0199456 220.9899 263.7348 12.93390913399505
| Epoch (UTC): | 22 December 2024 23:20:27 |
| Eccentricity: | 0.0199456 |
| inclination: | 102.5879° |
| perigee height: | 1135 km |
| apogee height: | 1441 km |
| right ascension of ascending node: | 127.8146° |
| argument of perigee: | 220.9899° |
| revolutions per day: | 12.93390913 |
| mean anomaly at epoch: | 263.7348° |
| orbit number at epoch: | 39950 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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