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 39382U 13064C 14295.69196181 .08127694 71009-5 39440-2 0 9992
2 39382 040.4749 030.1842 0010618 038.7078 321.6815 16.20014304 51948
| Epoch (UTC): | 22 October 2014 16:36:25 |
| Eccentricity: | 0.0010618 |
| inclination: | 40.4749° |
| perigee height: | 212 km |
| apogee height: | 226 km |
| right ascension of ascending node: | 30.1842° |
| argument of perigee: | 38.7078° |
| revolutions per day: | 16.20014304 |
| mean anomaly at epoch: | 321.6815° |
| orbit number at epoch: | 5194 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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