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 17295U 87003A 22146.07462723 .00005347 00000-0 26486-3 0 9996
2 17295 82.5124 167.6225 0003282 35.7235 324.4218 15.17564909932169
| Epoch (UTC): | 26 May 2022 01:47:27 |
| Eccentricity: | 0.0003282 |
| inclination: | 82.5124° |
| perigee height: | 511 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 167.6225° |
| argument of perigee: | 35.7235° |
| revolutions per day: | 15.17564909 |
| mean anomaly at epoch: | 324.4218° |
| orbit number at epoch: | 93216 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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