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 39483U 13076A 19017.18914923 .00000018 00000-0 61179-4 0 9996
2 39483 82.4840 56.3226 0018727 236.1823 123.7490 12.42888802229685
| Epoch (UTC): | 17 January 2019 04:32:22 |
| Eccentricity: | 0.0018727 |
| inclination: | 82.4840° |
| perigee height: | 1479 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 56.3226° |
| argument of perigee: | 236.1823° |
| revolutions per day: | 12.42888802 |
| mean anomaly at epoch: | 123.7490° |
| orbit number at epoch: | 22968 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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