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 17192U 86097B 22138.11867635 .00000436 00000-0 49782-4 0 9990
2 17192 82.5082 10.7050 0015616 304.0353 169.3667 14.83759881914957
| Epoch (UTC): | 18 May 2022 02:50:53 |
| Eccentricity: | 0.0015616 |
| inclination: | 82.5082° |
| perigee height: | 606 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 10.7050° |
| argument of perigee: | 304.0353° |
| revolutions per day: | 14.83759881 |
| mean anomaly at epoch: | 169.3667° |
| orbit number at epoch: | 91495 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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