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 22276U 92089B 25199.90523330 .00002662 00000-0 19703-3 0 9997
2 22276 20.2849 84.9696 0052290 138.8837 221.5544 14.94089714741758
| Epoch (UTC): | 18 July 2025 21:43:32 |
| Eccentricity: | 0.0052290 |
| inclination: | 20.2849° |
| perigee height: | 549 km |
| apogee height: | 621 km |
| right ascension of ascending node: | 84.9696° |
| argument of perigee: | 138.8837° |
| revolutions per day: | 14.94089714 |
| mean anomaly at epoch: | 221.5544° |
| orbit number at epoch: | 74175 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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