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 13342.42753350 .00000069 00000-0 11312-3 0 1709
2 00005 034.2493 007.3090 1848710 071.5850 307.6212 10.84377699946583
| Epoch (UTC): | 08 December 2013 10:15:38 |
| Eccentricity: | 0.1848710 |
| inclination: | 34.2493° |
| perigee height: | 650 km |
| apogee height: | 3838 km |
| right ascension of ascending node: | 7.3090° |
| argument of perigee: | 71.5850° |
| revolutions per day: | 10.84377699 |
| mean anomaly at epoch: | 307.6212° |
| orbit number at epoch: | 94658 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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