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 44443U 19043A 19217.68179789 .10560506 89749-5 36947-2 0 9997
2 44443 42.7194 295.4156 0012393 4.8471 131.9425 16.24009227 1843
| Epoch (UTC): | 05 August 2019 16:21:47 |
| Eccentricity: | 0.0012393 |
| inclination: | 42.7194° |
| perigee height: | 200 km |
| apogee height: | 217 km |
| right ascension of ascending node: | 295.4156° |
| argument of perigee: | 4.8471° |
| revolutions per day: | 16.24009227 |
| mean anomaly at epoch: | 131.9425° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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