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 00005U 58002B 18110.34567316 .00000046 00000-0 81934-4 0 9995
2 00005 34.2425 138.9261 1845823 41.6778 331.0652 10.84810709119651
| Epoch (UTC): | 20 April 2018 08:17:46 |
| Eccentricity: | 0.1845823 |
| inclination: | 34.2425° |
| perigee height: | 650 km |
| apogee height: | 3833 km |
| right ascension of ascending node: | 138.9261° |
| argument of perigee: | 41.6778° |
| revolutions per day: | 10.84810709 |
| mean anomaly at epoch: | 331.0652° |
| orbit number at epoch: | 11965 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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