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 14552U 83122B 14209.81484844 .00000292 00000-0 33042-4 0 9179
2 14552 082.5270 343.3961 0017952 039.7107 112.2580 14.82858846652896
| Epoch (UTC): | 28 July 2014 19:33:22 |
| Eccentricity: | 0.0017952 |
| inclination: | 82.5270° |
| perigee height: | 608 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 343.3961° |
| argument of perigee: | 39.7107° |
| revolutions per day: | 14.82858846 |
| mean anomaly at epoch: | 112.2580° |
| orbit number at epoch: | 65289 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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