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 18271.10377563 0.00000000 00000-0 00000-0 0 02
2 32287 4.9476 69.8277 0003304 221.7410 138.2457 1.00329927 03
| Epoch (UTC): | 28 September 2018 02:29:26 |
| Eccentricity: | 0.0003304 |
| inclination: | 4.9476° |
| perigee height: | 35756 km |
| apogee height: | 35784 km |
| right ascension of ascending node: | 69.8277° |
| argument of perigee: | 221.7410° |
| revolutions per day: | 1.00329927 |
| mean anomaly at epoch: | 138.2457° |
| 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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