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 15595U 85021A 18230.76333972 -.00000090 00000-0 14916-4 0 9990
2 15595 108.0365 262.6773 0002008 287.1720 202.0405 14.38082572751848
| Epoch (UTC): | 18 August 2018 18:19:12 |
| Eccentricity: | 0.0002008 |
| inclination: | 108.0365° |
| perigee height: | 763 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 262.6773° |
| argument of perigee: | 287.1720° |
| revolutions per day: | 14.38082572 |
| mean anomaly at epoch: | 202.0405° |
| orbit number at epoch: | 75184 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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