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 16623U 86014D 20342.46719032 .09853863 83719-5 34718-2 0 9990
2 16623 63.2353 11.7987 0030676 80.2192 280.2432 16.23315973 75080
| Epoch (UTC): | 07 December 2020 11:12:45 |
| Eccentricity: | 0.0030676 |
| inclination: | 63.2353° |
| perigee height: | 190 km |
| apogee height: | 231 km |
| right ascension of ascending node: | 11.7987° |
| argument of perigee: | 80.2192° |
| revolutions per day: | 16.23315973 |
| mean anomaly at epoch: | 280.2432° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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