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 19047.33984502 .00000079 00000-0 12065-4 0 9997
2 43188 97.7163 317.5288 0012161 59.0465 301.1950 14.96578973 56833
| Epoch (UTC): | 16 February 2019 08:09:22 |
| Eccentricity: | 0.0012161 |
| inclination: | 97.7163° |
| perigee height: | 569 km |
| apogee height: | 586 km |
| right ascension of ascending node: | 317.5288° |
| argument of perigee: | 59.0465° |
| revolutions per day: | 14.96578973 |
| mean anomaly at epoch: | 301.1950° |
| orbit number at epoch: | 5683 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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