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 14190.48269316 .00000187 00000-0 15194-4 0 1760
2 15392 021.4978 177.1220 1034849 249.5896 274.5721 12.45417332350047
| Epoch (UTC): | 09 July 2014 11:35:04 |
| Eccentricity: | 0.1034849 |
| inclination: | 21.4978° |
| perigee height: | 670 km |
| apogee height: | 2297 km |
| right ascension of ascending node: | 177.1220° |
| argument of perigee: | 249.5896° |
| revolutions per day: | 12.45417332 |
| mean anomaly at epoch: | 274.5721° |
| orbit number at epoch: | 35004 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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