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 38047U 12001B 16300.92863863 .18489825 26156-5 23054-3 0 9998
2 38047 97.3971 76.7789 0011130 260.8276 99.6698 16.49214973270564
| Epoch (UTC): | 26 October 2016 22:17:14 |
| Eccentricity: | 0.0011130 |
| inclination: | 97.3971° |
| perigee height: | 134 km |
| apogee height: | 148 km |
| right ascension of ascending node: | 76.7789° |
| argument of perigee: | 260.8276° |
| revolutions per day: | 16.49214973 |
| mean anomaly at epoch: | 99.6698° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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