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 18322.52047968 .00000145 00000-0 40940-4 0 9992
2 29050 72.0141 132.3750 0051794 292.5093 67.0581 14.58734219672297
| Epoch (UTC): | 18 November 2018 12:29:29 |
| Eccentricity: | 0.0051794 |
| inclination: | 72.0141° |
| perigee height: | 660 km |
| apogee height: | 734 km |
| right ascension of ascending node: | 132.3750° |
| argument of perigee: | 292.5093° |
| revolutions per day: | 14.58734219 |
| mean anomaly at epoch: | 67.0581° |
| orbit number at epoch: | 67229 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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