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 43466U 98067NP 20162.72983235 .07919004 12439-4 62785-3 0 9997
2 43466 51.6123 283.7308 0007318 301.8476 166.2040 16.39179723119460
| Epoch (UTC): | 10 June 2020 17:30:57 |
| Eccentricity: | 0.0007318 |
| inclination: | 51.6123° |
| perigee height: | 163 km |
| apogee height: | 173 km |
| right ascension of ascending node: | 283.7308° |
| argument of perigee: | 301.8476° |
| revolutions per day: | 16.39179723 |
| mean anomaly at epoch: | 166.2040° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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