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 39384U 13064E 15042.52146122 .08094018 00000-0 21500-2 0 9996
2 39384 040.4712 085.7529 0005450 293.5781 066.5269 16.27280585 69241
| Epoch (UTC): | 11 February 2015 12:30:54 |
| Eccentricity: | 0.0005450 |
| inclination: | 40.4712° |
| perigee height: | 196 km |
| apogee height: | 203 km |
| right ascension of ascending node: | 85.7529° |
| argument of perigee: | 293.5781° |
| revolutions per day: | 16.27280585 |
| mean anomaly at epoch: | 66.5269° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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