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 27431U 02024B 22144.91861869 .00000136 00000-0 10348-3 0 9995
2 27431 99.1324 165.1782 0016497 86.5594 273.7462 14.09764906 30315
| Epoch (UTC): | 24 May 2022 22:02:48 |
| Eccentricity: | 0.0016497 |
| inclination: | 99.1324° |
| perigee height: | 848 km |
| apogee height: | 872 km |
| right ascension of ascending node: | 165.1782° |
| argument of perigee: | 86.5594° |
| revolutions per day: | 14.09764906 |
| mean anomaly at epoch: | 273.7462° |
| orbit number at epoch: | 3031 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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