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 40392U 15008A 15168.23123306 +.00014817 +00000-0 +21985-3 0 9992
2 40392 051.6461 083.8018 0004336 062.0674 099.5751 15.55445497948042
| Epoch (UTC): | 17 June 2015 05:32:58 |
| Eccentricity: | 0.0004336 |
| inclination: | 51.6461° |
| perigee height: | 398 km |
| apogee height: | 404 km |
| right ascension of ascending node: | 83.8018° |
| argument of perigee: | 62.0674° |
| revolutions per day: | 15.55445497 |
| mean anomaly at epoch: | 99.5751° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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