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 32287U 07054A 18140.50942373 0.00000000 00000-0 00000-0 0 08
2 32287 4.7028 70.3110 0003530 203.7660 156.2299 1.00282207 08
| Epoch (UTC): | 20 May 2018 12:13:34 |
| Eccentricity: | 0.0003530 |
| inclination: | 4.7028° |
| perigee height: | 35768 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 70.3110° |
| argument of perigee: | 203.7660° |
| revolutions per day: | 1.00282207 |
| mean anomaly at epoch: | 156.2299° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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