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 18196.34383296 0.00000000 00000-0 00000-0 0 04
2 32287 4.8410 70.1348 0003723 207.2384 152.7544 1.00303816 05
| Epoch (UTC): | 15 July 2018 08:15:07 |
| Eccentricity: | 0.0003723 |
| inclination: | 4.8410° |
| perigee height: | 35761 km |
| apogee height: | 35793 km |
| right ascension of ascending node: | 70.1348° |
| argument of perigee: | 207.2384° |
| revolutions per day: | 1.00303816 |
| mean anomaly at epoch: | 152.7544° |
| 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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