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 22143.87262615 .00000257 00000-0 88273-4 0 9991
2 16864 74.0301 0.2308 0032745 13.7088 346.4949 14.40723105882108
| Epoch (UTC): | 23 May 2022 20:56:34 |
| Eccentricity: | 0.0032745 |
| inclination: | 74.0301° |
| perigee height: | 733 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 0.2308° |
| argument of perigee: | 13.7088° |
| revolutions per day: | 14.40723105 |
| mean anomaly at epoch: | 346.4949° |
| orbit number at epoch: | 88210 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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