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 18110.72615304 0.00000000 00000-0 00000-0 0 07
2 20929 15.4085 8.0076 0007831 327.4055 32.5582 0.98395838 01
| Epoch (UTC): | 20 April 2018 17:25:39 |
| Eccentricity: | 0.0007831 |
| inclination: | 15.4085° |
| perigee height: | 36287 km |
| apogee height: | 36354 km |
| right ascension of ascending node: | 8.0076° |
| argument of perigee: | 327.4055° |
| revolutions per day: | 0.98395838 |
| mean anomaly at epoch: | 32.5582° |
| 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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