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 22147.59274875 .00000189 00000-0 76014-4 0 9990
2 27386 98.1824 129.6801 0001287 87.6461 28.6981 14.38125602 60469
| Epoch (UTC): | 27 May 2022 14:13:33 |
| Eccentricity: | 0.0001287 |
| inclination: | 98.1824° |
| perigee height: | 764 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 129.6801° |
| argument of perigee: | 87.6461° |
| revolutions per day: | 14.38125602 |
| mean anomaly at epoch: | 28.6981° |
| orbit number at epoch: | 6046 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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