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 20929U 90095A 18217.43252132 0.00000000 00000-0 00000-0 0 09
2 20929 15.4150 7.0208 0006339 9.2556 350.7681 0.98393526 00
| Epoch (UTC): | 05 August 2018 10:22:49 |
| Eccentricity: | 0.0006339 |
| inclination: | 15.4150° |
| perigee height: | 36294 km |
| apogee height: | 36348 km |
| right ascension of ascending node: | 7.0208° |
| argument of perigee: | 9.2556° |
| revolutions per day: | 0.98393526 |
| mean anomaly at epoch: | 350.7681° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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