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 13719U 82116B 14110.84433425 .00000105 00000-0 46621-4 0 3981
2 13719 081.2567 050.1017 0072481 043.2783 008.5253 14.14455998617316
| Epoch (UTC): | 20 April 2014 20:15:50 |
| Eccentricity: | 0.0072481 |
| inclination: | 81.2567° |
| perigee height: | 792 km |
| apogee height: | 896 km |
| right ascension of ascending node: | 50.1017° |
| argument of perigee: | 43.2783° |
| revolutions per day: | 14.14455998 |
| mean anomaly at epoch: | 8.5253° |
| orbit number at epoch: | 61731 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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