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 39092U 13009G 17178.91370076 -.00000016 +00000-0 +98095-5 0 9997
2 39092 098.5505 023.3243 0008190 270.1695 089.8552 14.34905761227000
| Epoch (UTC): | 27 June 2017 21:55:43 |
| Eccentricity: | 0.0008190 |
| inclination: | 98.5505° |
| perigee height: | 769 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 23.3243° |
| argument of perigee: | 270.1695° |
| revolutions per day: | 14.34905761 |
| mean anomaly at epoch: | 89.8552° |
| orbit number at epoch: | 22700 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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