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 42722U 98067MB 19201.13118119 .02828887 12202-4 39331-3 0 9991
2 42722 51.6139 97.9553 0012743 244.1662 264.8455 16.33980456123504
| Epoch (UTC): | 20 July 2019 03:08:54 |
| Eccentricity: | 0.0012743 |
| inclination: | 51.6139° |
| perigee height: | 173 km |
| apogee height: | 190 km |
| right ascension of ascending node: | 97.9553° |
| argument of perigee: | 244.1662° |
| revolutions per day: | 16.33980456 |
| mean anomaly at epoch: | 264.8455° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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