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 42822U 98067MW 19131.43194823 .10190864 12355-4 76666-3 0 9990
2 42822 51.6054 100.7046 0005179 246.5694 204.7401 16.39672911105736
| Epoch (UTC): | 11 May 2019 10:22:00 |
| Eccentricity: | 0.0005179 |
| inclination: | 51.6054° |
| perigee height: | 163 km |
| apogee height: | 170 km |
| right ascension of ascending node: | 100.7046° |
| argument of perigee: | 246.5694° |
| revolutions per day: | 16.39672911 |
| mean anomaly at epoch: | 204.7401° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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