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 18350.87525326 +.00000019 +00000-0 +83984-5 0 9997
2 6153 035.0054 180.8460 0007324 220.4568 279.2730 14.57896669460588
| Epoch (UTC): | 16 December 2018 21:00:21 |
| Eccentricity: | 0.0007324 |
| inclination: | 35.0054° |
| perigee height: | 695 km |
| apogee height: | 705 km |
| right ascension of ascending node: | 180.8460° |
| argument of perigee: | 220.4568° |
| revolutions per day: | 14.57896669 |
| mean anomaly at epoch: | 279.2730° |
| orbit number at epoch: | 46058 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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