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 42016U 17008BW 18351.40502314 .00001105 00000-0 47220-4 0 9992
2 42016 97.4282 55.2021 0007997 95.1044 265.1106 15.24957233101966
| Epoch (UTC): | 17 December 2018 09:43:13 |
| Eccentricity: | 0.0007997 |
| inclination: | 97.4282° |
| perigee height: | 485 km |
| apogee height: | 496 km |
| right ascension of ascending node: | 55.2021° |
| argument of perigee: | 95.1044° |
| revolutions per day: | 15.24957233 |
| mean anomaly at epoch: | 265.1106° |
| orbit number at epoch: | 10196 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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