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 12586U 81065B 22144.90097803 .00003067 00000-0 18149-3 0 9993
2 12586 97.6833 139.1226 0019579 132.8506 227.4373 15.12058032224508
| Epoch (UTC): | 24 May 2022 21:37:24 |
| Eccentricity: | 0.0019579 |
| inclination: | 97.6833° |
| perigee height: | 516 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 139.1226° |
| argument of perigee: | 132.8506° |
| revolutions per day: | 15.12058032 |
| mean anomaly at epoch: | 227.4373° |
| orbit number at epoch: | 22450 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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