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 17228.91078762 +.00000008 +00000-0 +18055-4 0 9997
2 39092 098.5469 072.8163 0010412 117.7804 242.4438 14.34910622234175
| Epoch (UTC): | 16 August 2017 21:51:32 |
| Eccentricity: | 0.0010412 |
| inclination: | 98.5469° |
| perigee height: | 768 km |
| apogee height: | 783 km |
| right ascension of ascending node: | 72.8163° |
| argument of perigee: | 117.7804° |
| revolutions per day: | 14.34910622 |
| mean anomaly at epoch: | 242.4438° |
| orbit number at epoch: | 23417 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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