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 24283.81171267 .00012902 00000-0 63260-3 0 9990
2 19210 82.5121 313.3628 0015669 131.4225 228.8358 15.17902287959231
| Epoch (UTC): | 09 October 2024 19:28:51 |
| Eccentricity: | 0.0015669 |
| inclination: | 82.5121° |
| perigee height: | 501 km |
| apogee height: | 523 km |
| right ascension of ascending node: | 313.3628° |
| argument of perigee: | 131.4225° |
| revolutions per day: | 15.17902287 |
| mean anomaly at epoch: | 228.8358° |
| orbit number at epoch: | 95923 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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