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 16495U 86006A 18114.10204027 .00000930 00000-0 37091-4 0 9992
2 16495 82.4705 119.1348 0013079 177.2060 182.9252 15.23838945763657
| Epoch (UTC): | 24 April 2018 02:26:56 |
| Eccentricity: | 0.0013079 |
| inclination: | 82.4705° |
| perigee height: | 485 km |
| apogee height: | 503 km |
| right ascension of ascending node: | 119.1348° |
| argument of perigee: | 177.2060° |
| revolutions per day: | 15.23838945 |
| mean anomaly at epoch: | 182.9252° |
| orbit number at epoch: | 76365 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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