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 00005U 58002B 14200.70102250 -.00000104 00000-0 -12159-3 0 2423
2 00005 034.2486 039.9565 1849244 355.5651 003.0393 10.84388147970809
| Epoch (UTC): | 19 July 2014 16:49:28 |
| Eccentricity: | 0.1849244 |
| inclination: | 34.2486° |
| perigee height: | 649 km |
| apogee height: | 3838 km |
| right ascension of ascending node: | 39.9565° |
| argument of perigee: | 355.5651° |
| revolutions per day: | 10.84388147 |
| mean anomaly at epoch: | 3.0393° |
| orbit number at epoch: | 97080 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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