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 6153U 72065A 19345.35081160 .00000025 00000-0 98248-5 0 9994
2 6153 35.0076 299.6187 0007409 266.1177 227.4674 14.57928078513349
| Epoch (UTC): | 11 December 2019 08:25:10 |
| Eccentricity: | 0.0007409 |
| inclination: | 35.0076° |
| perigee height: | 694 km |
| apogee height: | 705 km |
| right ascension of ascending node: | 299.6187° |
| argument of perigee: | 266.1177° |
| revolutions per day: | 14.57928078 |
| mean anomaly at epoch: | 227.4674° |
| orbit number at epoch: | 51334 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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