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 14781U 84021B 14114.40737445 .00001165 00000-0 15513-3 0 4728
2 14781 097.8573 175.5697 0008249 005.7899 354.3407 14.81523422620009
| Epoch (UTC): | 24 April 2014 09:46:37 |
| Eccentricity: | 0.0008249 |
| inclination: | 97.8573° |
| perigee height: | 619 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 175.5697° |
| argument of perigee: | 5.7899° |
| revolutions per day: | 14.81523422 |
| mean anomaly at epoch: | 354.3407° |
| orbit number at epoch: | 62000 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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