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 38852U 98067CN 13218.07382584 .24681979 12625-4 36599-3 0 9999
2 38852 051.6160 184.0336 0004489 261.9162 100.6538 16.48474690 47849
| Epoch (UTC): | 06 August 2013 01:46:18 |
| Eccentricity: | 0.0004489 |
| inclination: | 51.6160° |
| perigee height: | 140 km |
| apogee height: | 146 km |
| right ascension of ascending node: | 184.0336° |
| argument of perigee: | 261.9162° |
| revolutions per day: | 16.48474690 |
| mean anomaly at epoch: | 100.6538° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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