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 19210U 88050A 24284.53685370 .00014344 00000-0 70289-3 0 9996
2 19210 82.5120 312.6453 0015669 129.0433 231.2198 15.17924831959343
| Epoch (UTC): | 10 October 2024 12:53:04 |
| Eccentricity: | 0.0015669 |
| inclination: | 82.5120° |
| perigee height: | 501 km |
| apogee height: | 523 km |
| right ascension of ascending node: | 312.6453° |
| argument of perigee: | 129.0433° |
| revolutions per day: | 15.17924831 |
| mean anomaly at epoch: | 231.2198° |
| orbit number at epoch: | 95934 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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