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 4256U 69082B 19287.81359593 .00000033 00000-0 60211-4 0 9992
2 4256 70.0091 156.1977 0019238 6.3362 353.7984 13.98338610549666
| Epoch (UTC): | 14 October 2019 19:31:34 |
| Eccentricity: | 0.0019238 |
| inclination: | 70.0091° |
| perigee height: | 885 km |
| apogee height: | 913 km |
| right ascension of ascending node: | 156.1977° |
| argument of perigee: | 6.3362° |
| revolutions per day: | 13.98338610 |
| mean anomaly at epoch: | 353.7984° |
| orbit number at epoch: | 54966 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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