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 23789U 96009C 19016.90340642 .00000029 00000-0 10294-3 0 9998
2 23789 82.5780 248.8751 0005905 78.2079 281.9673 12.62601998 55918
| Epoch (UTC): | 16 January 2019 21:40:54 |
| Eccentricity: | 0.0005905 |
| inclination: | 82.5780° |
| perigee height: | 1407 km |
| apogee height: | 1417 km |
| right ascension of ascending node: | 248.8751° |
| argument of perigee: | 78.2079° |
| revolutions per day: | 12.62601998 |
| mean anomaly at epoch: | 281.9673° |
| orbit number at epoch: | 5591 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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