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 is defined by the following mean orbital elements,
1 42725U 98067ME 19087.71781172 .15670676 12603-4 45746-3 0 9992
2 42725 51.6064 319.7683 0009359 299.6698 60.5570 16.44549673105565
| Epoch (UTC): | 28 March 2019 17:13:38 |
| Eccentricity: | 0.0009359 |
| inclination: | 51.6064° |
| perigee height: | 147 km |
| apogee height: | 160 km |
| right ascension of ascending node: | 319.7683° |
| argument of perigee: | 299.6698° |
| revolutions per day: | 16.44549673 |
| mean anomaly at epoch: | 60.5570° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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