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 29048U 06011B 18231.64475663 -.00000015 00000-0 10263-4 0 9990
2 29048 71.9675 304.5737 0042002 89.6678 270.9271 14.28584219648438
| Epoch (UTC): | 19 August 2018 15:28:26 |
| Eccentricity: | 0.0042002 |
| inclination: | 71.9675° |
| perigee height: | 766 km |
| apogee height: | 826 km |
| right ascension of ascending node: | 304.5737° |
| argument of perigee: | 89.6678° |
| revolutions per day: | 14.28584219 |
| mean anomaly at epoch: | 270.9271° |
| orbit number at epoch: | 64843 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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