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 19054.53628709 -.00000089 00000-0 15146-4 0 9999
2 15595 108.0333 294.1420 0001701 295.2631 127.2249 14.38103532778980
| Epoch (UTC): | 23 February 2019 12:52:15 |
| Eccentricity: | 0.0001701 |
| inclination: | 108.0333° |
| perigee height: | 763 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 294.1420° |
| argument of perigee: | 295.2631° |
| revolutions per day: | 14.38103532 |
| mean anomaly at epoch: | 127.2249° |
| orbit number at epoch: | 77898 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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