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 40292U 14067A 15116.18326566 .00016849 00000-0 24679-3 0 9995
2 40292 051.6481 343.8143 0003434 274.9158 179.9634 15.55687816 27819
| Epoch (UTC): | 26 April 2015 04:23:54 |
| Eccentricity: | 0.0003434 |
| inclination: | 51.6481° |
| perigee height: | 398 km |
| apogee height: | 402 km |
| right ascension of ascending node: | 343.8143° |
| argument of perigee: | 274.9158° |
| revolutions per day: | 15.55687816 |
| mean anomaly at epoch: | 179.9634° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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