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 22179.59773328 .00000051 00000-0 30468-4 0 9993
2 27386 98.1836 160.1828 0001345 90.5415 27.8563 14.38134952 65064
| Epoch (UTC): | 28 June 2022 14:20:44 |
| Eccentricity: | 0.0001345 |
| inclination: | 98.1836° |
| perigee height: | 764 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 160.1828° |
| argument of perigee: | 90.5415° |
| revolutions per day: | 14.38134952 |
| mean anomaly at epoch: | 27.8563° |
| orbit number at epoch: | 6506 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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