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 39404U 13064AA 17304.93805027 .14819696 74099-5 47644-3 0 9999
2 39404 40.4789 145.0538 0001854 314.5146 47.1024 16.45154788222993
| Epoch (UTC): | 31 October 2017 22:30:47 |
| Eccentricity: | 0.0001854 |
| inclination: | 40.4789° |
| perigee height: | 151 km |
| apogee height: | 153 km |
| right ascension of ascending node: | 145.0538° |
| argument of perigee: | 314.5146° |
| revolutions per day: | 16.45154788 |
| mean anomaly at epoch: | 47.1024° |
| orbit number at epoch: | 22299 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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