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 27386U 02009A 22140.71575241 .00000325 00000-0 12075-3 0 9996
2 27386 98.1820 123.1264 0001326 86.5060 86.6491 14.38121642 59541
| Epoch (UTC): | 20 May 2022 17:10:41 |
| Eccentricity: | 0.0001326 |
| inclination: | 98.1820° |
| perigee height: | 764 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 123.1264° |
| argument of perigee: | 86.5060° |
| revolutions per day: | 14.38121642 |
| mean anomaly at epoch: | 86.6491° |
| orbit number at epoch: | 5954 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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