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 39762U 14028B 17268.91295989 +.00000010 +00000-0 +00000-0 0 9999
2 39762 082.4504 305.0140 0020691 168.3824 191.7742 12.42869037151768
| Epoch (UTC): | 25 September 2017 21:54:39 |
| Eccentricity: | 0.0020691 |
| inclination: | 82.4504° |
| perigee height: | 1478 km |
| apogee height: | 1511 km |
| right ascension of ascending node: | 305.0140° |
| argument of perigee: | 168.3824° |
| revolutions per day: | 12.42869037 |
| mean anomaly at epoch: | 191.7742° |
| orbit number at epoch: | 15176 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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