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 15392U 84115B 15063.59313956 .00000172 00000-0 25984-4 0 9997
2 15392 021.4906 169.2734 1034756 035.4448 105.6422 12.45477594379759
| Epoch (UTC): | 04 March 2015 14:14:07 |
| Eccentricity: | 0.1034756 |
| inclination: | 21.4906° |
| perigee height: | 670 km |
| apogee height: | 2297 km |
| right ascension of ascending node: | 169.2734° |
| argument of perigee: | 35.4448° |
| revolutions per day: | 12.45477594 |
| mean anomaly at epoch: | 105.6422° |
| orbit number at epoch: | 37975 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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