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 14106.04450764 .00000385 00000-0 15225-3 0 3457
2 39092 098.6214 300.6737 0009963 127.6622 232.5464 14.34541175 59414
| Epoch (UTC): | 16 April 2014 01:04:05 |
| Eccentricity: | 0.0009963 |
| inclination: | 98.6214° |
| perigee height: | 769 km |
| apogee height: | 784 km |
| right ascension of ascending node: | 300.6737° |
| argument of perigee: | 127.6622° |
| revolutions per day: | 14.34541175 |
| mean anomaly at epoch: | 232.5464° |
| orbit number at epoch: | 5941 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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