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 39062U 13002B 19051.09200797 .17883199 26807-5 27012-3 0 9995
2 39062 97.1725 179.4823 0005582 143.2824 217.8108 16.48581280342482
| Epoch (UTC): | 20 February 2019 02:12:29 |
| Eccentricity: | 0.0005582 |
| inclination: | 97.1725° |
| perigee height: | 139 km |
| apogee height: | 147 km |
| right ascension of ascending node: | 179.4823° |
| argument of perigee: | 143.2824° |
| revolutions per day: | 16.48581280 |
| mean anomaly at epoch: | 217.8108° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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