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 43188U 18014J 19341.17815198 .00000035 00000-0 81327-5 0 9990
2 43188 97.7023 247.0449 0011743 144.3965 215.8042 14.96722987100785
| Epoch (UTC): | 07 December 2019 04:16:32 |
| Eccentricity: | 0.0011743 |
| inclination: | 97.7023° |
| perigee height: | 569 km |
| apogee height: | 585 km |
| right ascension of ascending node: | 247.0449° |
| argument of perigee: | 144.3965° |
| revolutions per day: | 14.96722987 |
| mean anomaly at epoch: | 215.8042° |
| orbit number at epoch: | 10078 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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