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 22183.90048176 .00000039 00000-0 26274-4 0 9995
2 27386 98.1837 164.2840 0001341 90.5102 331.4946 14.38135675 65751
| Epoch (UTC): | 02 July 2022 21:36:41 |
| Eccentricity: | 0.0001341 |
| inclination: | 98.1837° |
| perigee height: | 764 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 164.2840° |
| argument of perigee: | 90.5102° |
| revolutions per day: | 14.38135675 |
| mean anomaly at epoch: | 331.4946° |
| orbit number at epoch: | 6575 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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