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 29050U 06011D 19340.57116908 +.00000072 +00000-0 +25645-4 0 9993
2 29050 072.0169 033.2915 0051664 315.3310 044.3685 14.58860463728051
| Epoch (UTC): | 06 December 2019 13:42:29 |
| Eccentricity: | 0.0051664 |
| inclination: | 72.0169° |
| perigee height: | 660 km |
| apogee height: | 733 km |
| right ascension of ascending node: | 33.2915° |
| argument of perigee: | 315.3310° |
| revolutions per day: | 14.58860463 |
| mean anomaly at epoch: | 44.3685° |
| orbit number at epoch: | 72805 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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