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 40713U 15031A 15352.54319571 +.00014358 +00000-0 +21741-3 0 9995
2 40713 051.6437 244.0274 0008333 295.0996 127.4199 15.54892795976722
| Epoch (UTC): | 18 December 2015 13:02:12 |
| Eccentricity: | 0.0008333 |
| inclination: | 51.6437° |
| perigee height: | 397 km |
| apogee height: | 408 km |
| right ascension of ascending node: | 244.0274° |
| argument of perigee: | 295.0996° |
| revolutions per day: | 15.54892795 |
| mean anomaly at epoch: | 127.4199° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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