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 22148.75316109 .00002176 00000-0 13758-3 0 9997
2 16986 82.5013 162.0503 0011014 333.9567 26.1106 15.08513003921791
| Epoch (UTC): | 28 May 2022 18:04:33 |
| Eccentricity: | 0.0011014 |
| inclination: | 82.5013° |
| perigee height: | 533 km |
| apogee height: | 548 km |
| right ascension of ascending node: | 162.0503° |
| argument of perigee: | 333.9567° |
| revolutions per day: | 15.08513003 |
| mean anomaly at epoch: | 26.1106° |
| orbit number at epoch: | 92179 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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