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 37169U 10048B 22230.08386030 .00007013 00000-0 22304-3 0 9991
2 37169 98.0058 46.0567 0005605 19.7409 340.4047 15.32952854660886
| Epoch (UTC): | 18 August 2022 02:00:45 |
| Eccentricity: | 0.0005605 |
| inclination: | 98.0058° |
| perigee height: | 463 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 46.0567° |
| argument of perigee: | 19.7409° |
| revolutions per day: | 15.32952854 |
| mean anomaly at epoch: | 340.4047° |
| orbit number at epoch: | 66088 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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