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 data is extracted from the following two-line orbital elements,
1 40619U 15024A 15127.81228385 .06736651 12531-4 10653-3 0 9993
2 40619 051.6438 280.6115 0008840 127.8365 232.4708 16.47715957 1553
| Epoch (UTC): | 07 May 2015 19:29:41 |
| Eccentricity: | 0.0008840 |
| inclination: | 51.6438° |
| perigee height: | 139 km |
| apogee height: | 151 km |
| right ascension of ascending node: | 280.6115° |
| argument of perigee: | 127.8365° |
| revolutions per day: | 16.47715957 |
| mean anomaly at epoch: | 232.4708° |
| orbit number at epoch: | 155 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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