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 18175.84762321 .00001674 00000-0 71141-4 0 9990
2 42016 97.4478 240.8527 0006403 8.8939 351.2411 15.24447944 75218
| Epoch (UTC): | 24 June 2018 20:20:34 |
| Eccentricity: | 0.0006403 |
| inclination: | 97.4478° |
| perigee height: | 488 km |
| apogee height: | 497 km |
| right ascension of ascending node: | 240.8527° |
| argument of perigee: | 8.8939° |
| revolutions per day: | 15.24447944 |
| mean anomaly at epoch: | 351.2411° |
| orbit number at epoch: | 7521 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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