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 data is extracted from the following two-line orbital elements,
1 16496U 86006B 21110.60657369 .00000105 00000-0 96441-5 0 9998
2 16496 82.5226 134.2605 0020688 115.2407 6.5220 14.84177981884407
| Epoch (UTC): | 20 April 2021 14:33:27 |
| Eccentricity: | 0.0020688 |
| inclination: | 82.5226° |
| perigee height: | 602 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 134.2605° |
| argument of perigee: | 115.2407° |
| revolutions per day: | 14.84177981 |
| mean anomaly at epoch: | 6.5220° |
| orbit number at epoch: | 88440 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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