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 16273.09880555 .00000042 00000-0 30204-4 0 9994
2 39092 98.5715 113.8510 0009457 2.6832 357.4403 14.34866967188035
| Epoch (UTC): | 29 September 2016 02:22:16 |
| Eccentricity: | 0.0009457 |
| inclination: | 98.5715° |
| perigee height: | 769 km |
| apogee height: | 782 km |
| right ascension of ascending node: | 113.8510° |
| argument of perigee: | 2.6832° |
| revolutions per day: | 14.34866967 |
| mean anomaly at epoch: | 357.4403° |
| orbit number at epoch: | 18803 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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