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 29079U 06014A 18293.86500839 .00001635 00000-0 72306-4 0 9997
2 29079 97.3995 50.7337 0001735 251.8931 222.3698 15.23106413693030
| Epoch (UTC): | 20 October 2018 20:45:36 |
| Eccentricity: | 0.0001735 |
| inclination: | 97.3995° |
| perigee height: | 495 km |
| apogee height: | 497 km |
| right ascension of ascending node: | 50.7337° |
| argument of perigee: | 251.8931° |
| revolutions per day: | 15.23106413 |
| mean anomaly at epoch: | 222.3698° |
| orbit number at epoch: | 69303 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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