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 42727U 98067MG 19089.91797841 .06519165 12339-4 59073-3 0 9997
2 42727 51.6087 308.8243 0009316 268.9251 91.0707 16.37980460105869
| Epoch (UTC): | 30 March 2019 22:01:53 |
| Eccentricity: | 0.0009316 |
| inclination: | 51.6087° |
| perigee height: | 165 km |
| apogee height: | 177 km |
| right ascension of ascending node: | 308.8243° |
| argument of perigee: | 268.9251° |
| revolutions per day: | 16.37980460 |
| mean anomaly at epoch: | 91.0707° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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