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 16986U 86074A 22140.52785884 .00003263 00000-0 20739-3 0 9999
2 16986 82.5036 170.0787 0011500 0.0434 0.0793 15.08470107920557
| Epoch (UTC): | 20 May 2022 12:40:07 |
| Eccentricity: | 0.0011500 |
| inclination: | 82.5036° |
| perigee height: | 533 km |
| apogee height: | 549 km |
| right ascension of ascending node: | 170.0787° |
| argument of perigee: | 0.0434° |
| revolutions per day: | 15.08470107 |
| mean anomaly at epoch: | 0.0793° |
| orbit number at epoch: | 92055 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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