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 20179.95692127 0.00000000 00000-0 00000-0 0 04
2 23567 14.9350 27.5947 0033875 83.0409 277.3632 1.00270000 01
| Epoch (UTC): | 27 June 2020 22:57:57 |
| Eccentricity: | 0.0033875 |
| inclination: | 14.9350° |
| perigee height: | 35644 km |
| apogee height: | 35929 km |
| right ascension of ascending node: | 27.5947° |
| argument of perigee: | 83.0409° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 277.3632° |
| 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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