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 16864U 86052B 22139.91468876 .00000356 00000-0 11903-3 0 9993
2 16864 74.0306 7.5560 0032587 22.2103 338.0455 14.40720949881538
| Epoch (UTC): | 19 May 2022 21:57:09 |
| Eccentricity: | 0.0032587 |
| inclination: | 74.0306° |
| perigee height: | 733 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 7.5560° |
| argument of perigee: | 22.2103° |
| revolutions per day: | 14.40720949 |
| mean anomaly at epoch: | 338.0455° |
| orbit number at epoch: | 88153 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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