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 14109.69129234 .00000047 00000-0 46413-4 0 2122
2 00005 034.2553 320.1507 1850173 306.3250 038.0075 10.84394864960949
| Epoch (UTC): | 19 April 2014 16:35:27 |
| Eccentricity: | 0.1850173 |
| inclination: | 34.2553° |
| perigee height: | 648 km |
| apogee height: | 3839 km |
| right ascension of ascending node: | 320.1507° |
| argument of perigee: | 306.3250° |
| revolutions per day: | 10.84394864 |
| mean anomaly at epoch: | 38.0075° |
| orbit number at epoch: | 96094 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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