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 19081.81597362 +.00000041 +00000-0 +13294-4 0 9993
2 6153 035.0081 356.0710 0007521 275.7879 185.7396 14.57904311474599
| Epoch (UTC): | 22 March 2019 19:35:00 |
| Eccentricity: | 0.0007521 |
| inclination: | 35.0081° |
| perigee height: | 694 km |
| apogee height: | 705 km |
| right ascension of ascending node: | 356.0710° |
| argument of perigee: | 275.7879° |
| revolutions per day: | 14.57904311 |
| mean anomaly at epoch: | 185.7396° |
| orbit number at epoch: | 47459 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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