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 is defined by the following mean orbital elements,
1 38853U 98067CP 13184.86912902 .06638326 12312-4 50483-3 0 9991
2 38853 051.6252 351.6077 0011722 245.9321 114.2104 16.39337660 42708
| Epoch (UTC): | 03 July 2013 20:51:32 |
| Eccentricity: | 0.0011722 |
| inclination: | 51.6252° |
| perigee height: | 160 km |
| apogee height: | 175 km |
| right ascension of ascending node: | 351.6077° |
| argument of perigee: | 245.9321° |
| revolutions per day: | 16.39337660 |
| mean anomaly at epoch: | 114.2104° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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