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 40457U 98067GA 15213.38588329 .08885032 12472-4 72013-3 0 9998
2 40457 051.6142 195.6182 0009646 310.7124 049.3640 16.38908268 33335
| Epoch (UTC): | 01 August 2015 09:15:40 |
| Eccentricity: | 0.0009646 |
| inclination: | 51.6142° |
| perigee height: | 162 km |
| apogee height: | 175 km |
| right ascension of ascending node: | 195.6182° |
| argument of perigee: | 310.7124° |
| revolutions per day: | 16.38908268 |
| mean anomaly at epoch: | 49.3640° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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