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 23788U 96009B 19017.06996225 .00000005 00000-0 -31731-4 0 9994
2 23788 82.5690 237.1110 0007319 89.5667 270.6260 12.63144333 56404
| Epoch (UTC): | 17 January 2019 01:40:44 |
| Eccentricity: | 0.0007319 |
| inclination: | 82.5690° |
| perigee height: | 1404 km |
| apogee height: | 1415 km |
| right ascension of ascending node: | 237.1110° |
| argument of perigee: | 89.5667° |
| revolutions per day: | 12.63144333 |
| mean anomaly at epoch: | 270.6260° |
| orbit number at epoch: | 5640 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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