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 23567U 95022A 18342.52722876 0.00000000 00000-0 00000-0 0 01
2 23567 14.4292 33.2523 0057867 96.7775 263.8995 1.00270000 01
| Epoch (UTC): | 08 December 2018 12:39:12 |
| Eccentricity: | 0.0057867 |
| inclination: | 14.4292° |
| perigee height: | 35543 km |
| apogee height: | 36031 km |
| right ascension of ascending node: | 33.2523° |
| argument of perigee: | 96.7775° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 263.8995° |
| 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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