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 42824U 98067MY 19133.12526632 .12220275 12529-4 51637-3 0 9993
2 42824 51.6091 92.5367 0003545 299.4874 174.6355 16.43636834105973
| Epoch (UTC): | 13 May 2019 03:00:23 |
| Eccentricity: | 0.0003545 |
| inclination: | 51.6091° |
| perigee height: | 154 km |
| apogee height: | 158 km |
| right ascension of ascending node: | 92.5367° |
| argument of perigee: | 299.4874° |
| revolutions per day: | 16.43636834 |
| mean anomaly at epoch: | 174.6355° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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