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 22140.30537617 .00000004 00000-0 28105-4 0 9990
2 27431 99.1329 160.4975 0016473 98.5086 261.7951 14.09763901 29665
| Epoch (UTC): | 20 May 2022 07:19:44 |
| Eccentricity: | 0.0016473 |
| inclination: | 99.1329° |
| perigee height: | 848 km |
| apogee height: | 872 km |
| right ascension of ascending node: | 160.4975° |
| argument of perigee: | 98.5086° |
| revolutions per day: | 14.09763901 |
| mean anomaly at epoch: | 261.7951° |
| orbit number at epoch: | 2966 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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