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 18171.61674051 .00000028 00000-0 97817-4 0 9996
2 23788 82.5691 11.7644 0005746 205.0172 155.0629 12.63142438 29837
| Epoch (UTC): | 20 June 2018 14:48:06 |
| Eccentricity: | 0.0005746 |
| inclination: | 82.5691° |
| perigee height: | 1405 km |
| apogee height: | 1414 km |
| right ascension of ascending node: | 11.7644° |
| argument of perigee: | 205.0172° |
| revolutions per day: | 12.63142438 |
| mean anomaly at epoch: | 155.0629° |
| orbit number at epoch: | 2983 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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